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Airframes

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• Structural frames
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• Aircraft stress analysis
• Aircraft structures
• Air frames
• Airplanes -- Stresses
• Airplanes -- Structures

• Gain selection method and model for coupled propulsion and airframe systems / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Patrick C. Murphy and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Military handbook of aircraft extruded shapes and dies. (Washington : U. S. Govt. Print. Off., 1959), by United States Department of Defense (page images at HathiTrust)
• Sonic fatigue design techniques for advanced composite aircraft structures : final report / (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, [1980]), by I. Holehouse and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Critical combinations of shear and transverse direct stress for an infinitely long flat plate with edges elastically restrained against rotation / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1945), by S. B. Batdorf, John C. Houbolt, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• Frequency of occurrence of atmospheric gusts and of related loads on airplane structures / (Langley Field, VA : Langley Memorial Aeronautical Laboratory, 1944), by Richard V. Rhode, Philip Donely, United States. National Advisory Committee for Aeronautics, and Langley Aeronautical Laboratory (page images at HathiTrust)
• General aviation crashworthiness project. (Washington, D.C. : The Board ; Springfield, Va. : National Technical Information Service, [1983]), by United States. National Transportation Safety Board (page images at HathiTrust)
• Fatigue of aircraft structures, ([Washington, For sale by the Supt. of Docs., U. S. Govt. Print. Off.], 1966 [i. e. 1967]), by H. J. Grover, United States. Naval Air Systems Command, and Battelle Memorial Institute (page images at HathiTrust)
• The First Joint DoD/FAA/NASA Conference on Aging Aircraft : 8-10 July 1997, the David Eccles Conference Center, Odgen, Utah : proceedings / ([Washington, D.C.?] : U.S. G.P.O., [1998]), by Utah) Joint DoD/FAA/NASA Conference on Aging Aircraft (1st : 1997 : Ogden, J. P. Gallagher, U.S. Army Research Laboratory, Naval Air Warfare Center (U.S.), Ohio) Air Force Research Laboratory (Wright-Patterson Air Force Base, United States Federal Aviation Administration, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Elevated-temperature tests under static and aerodynamic conditions on honeycomb-core sandwich panels / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Joseph M. Groen, Aldie E. Johnson, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Design of a convective cooling system for a Mach 6 hypersonic transport airframe / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service [distributor], 1971), by R. G. Helenbrook, F. M. Anthony, Langley Research Center, and Bell Aerospace Company (page images at HathiTrust)
• Development and applications of two computational procedures for determining the vibration modes of structural systems / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Raymond G. Kvaternik and Langley Research Center (page images at HathiTrust)
• Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1971-1973), by S. Oken, Langley Research Center, Boeing Commercial Airplane Company, Boeing Company, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Evaluation of energy absorption of new concepts of aircraft composite subfloor intersections / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Lisa E. Jones, Huey D. Carden, and Langley Research Center (page images at HathiTrust)
• Elevated-temperature tests under static and aerodynamic conditions on corrugated-stiffened panels / (Washington [D.C.] : National Aeronautics and Space Administration, [1959]), by Joseph M. Groen, Richard Rosecrans, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Exploratory studies of mechanical cycling fatigue behavior of materials for the supersonic transport / (Washington : National Aeronautics and Space Administration : Springfield, Va. : for sale by the National Technical Information Service, 1964), by D. N. Gideon, W. S. Hyler, F. C. Holden, C. W. Marschall, United States National Aeronautics and Space Administration, and Battelle Memorial Institute (page images at HathiTrust)
• Aircraft propeller induced structure-borne noise / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by James F. Unruh, Langley Research Center, and Southwest Research Institute (page images at HathiTrust)
• Analysis of an emergency deceleration and descent of the XB-70-1 airplane due to engine damage resulting from structural failure / (Washington, D.C. : National Aeronautics and Space Administration, [1966]), by Chester H. Wolowicz and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A protection and detection surface (PADS) for damage tolerance / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1990), by Mark J. Shuart, Sherrill B. Biggers, Chunchu B. Prasad, and Lewis Research Center (page images at HathiTrust)
• Scatter factor and reliability of aircraft structures / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1972), by Gerhart I. Schuëller, Alfred Martin Freudenthal, Langley Research Center, and George Washington University (page images at HathiTrust)
• Prediction of airframe noise / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Jay C. Hardin and Langley Research Center (page images at HathiTrust)
• Investigation of aluminum phosphate coatings for thermal insulation of airframes / (Washington, [D.C.] : National Aeronautics and Space Administration, 1959), by A. G. Eubanks, D. G. Moore, and United States. National Bureau of Standards (page images at HathiTrust)
• Potential structural materials and design concepts for light aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1969), by Ladislao Pazmany, Inc San Diego Aircraft Engineering, NASA Headquarters Mission Analysis Division, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by James C. Williams, John N. Perkins, Delbert C. Summey, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• A study of NACA and NASA published information of pertinence in the design of light aircraft. (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information [distributor], 1970), by Clifford J. Moore, Dennis M. Phillips, Langley Research Center, and North Carolina State University. Dept. of Mechanical and Aerospace Engineering (page images at HathiTrust)
• Flutter at very high speeds / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Harry L. Runyan, Homer G. Morgan, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Reliability-based econometrics of aerospace structural systems : design criteria and test options / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by National Technical Information Service], 1974), by Jerrell M. Thomas, S. V. Hanagud, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Service evaluation of aluminum brazed titanium (ABTi) jet engine tailpipe extensions / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by S. D. Elrod, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Calculation of three-dimensional, inviscid supersonic, steady flows / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Gino Moretti, Langley Research Center, Polytechnic Institute of New York, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Evaluation of a strain-gage load calibration on a low-aspect-ratio wing structure at elevated temperature / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, VA : For sale by the National Technical Information Service, 1989), by Lawrence F. Reardon (page images at HathiTrust)
• A study of temperatures attained in a dummy aircraft wing during the summer at Madison, Wisconsin / (Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [1943]), by F. L. Browne, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Summary of a study of temperatures attained in a dummy aircraft wing during the summer at Madison, Wisconsin / (Madison, Wis. : U.S. Dept. of Agriculture, Forest Service, Forest Products Laboratory, [1943]), by F. L. Browne, University of Wisconsin, and Forest Products Laboratory (U.S.) (page images at HathiTrust)
• Surface modeling, grid generation, and related issues in computational fluid dynamic (CFD) solutions : proceedings of a workshop / ([Washington, D.C.] : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995), by Grid Generation NASA Workshop on Surface Modeling, United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, and United States. National Aeronautics and Space Administration Steering Committee on Surface Modeling and Grid Generation (page images at HathiTrust)
• Computational structures technology for airframes and propulsion systems : proceedings of two workshops sponsored by the National Aeronautics and Space Administration, Washington, D.C., and the Center for Computational Structures Technology, University of Virginia, Hampton, Virginia, and held at Lewis Research Center, Cleveland, Ohio, June 26-27, 1991, and at Langley Research Center, Hampton, Virginia, September 4-5, 1991 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992), by Ahmed Khairy Noor, Langley Research Center, University of Virginia. Center for Computational Structures Technology, United States National Aeronautics and Space Administration, Workshop on Computational Structures Technology for Airframes and Propulsion Systems (1991 : Langley Research Center), and Workshop on Computational Structures Technology for Airframes and Propulsion Systems (1991 : Lewis Research Center) (page images at HathiTrust)
• Recent advances in structures for hypersonic flight : proceedings of a symposium held at Langley Research Center, Hampton, Virginia, September 6-8, 1978. ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : for sale by the National Technical Information Service], 1978 [i.e. 1979]), by NASA Symposium on Recent Advances in Structures for Hypersonic Flight (1978 : Langley Research Center) (page images at HathiTrust)
• Composite repairs of cracked metallic airframe structures / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1993]), by Satya N. Atluri, John A. Volpe National Transportation Systems Center (U.S.), Aeronautical Research Laboratories (Australia), Knowledge Systems Inc, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Impact damage characterization and damage tolerance of composite sandwich airframe structures / [John S. Tomblin ... et al.] (Washington, D.C. : Office of Aviation Research, U.S. Federal Aviation Administration ; [Springfield, Va. : Available through the National Technical Information Service, 2001]), by John S. Tomblin, Wichita State University. Department of Aerospace Engineering, William J. Hughes Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Characterization of early stages of corrosion fatigue aircraft skin / (Washington, D.C. : U.S. Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by C. G. Schmidt, SRI International, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• The role of fretting fatigue on aircraft rivet hole cracking / (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by David W. Heoppner, University of Utah. Department of Mechanical Engineering, and United States. Office of Aviation Research (page images at HathiTrust)
• Lightning simulation test technique evaluation / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1988]), by William W. Cooley, Deborah L. Shortess, Inc Science & Engineering Associates, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Structural response to discrete and continuous gusts of an airplane having wing-bending flexibility and a correlation of calculated and flight results / (Washington, D.C. : U.S. Government Printing Office, 1954), by John C. Houbolt, Eldon E. Kordes, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Proceedings of the Air Force Conference on Fatigue and Fracture of Aircraft Structures and Materials : proceedings of the conference held at Miami Beach, Florida, 15-18 December 1969 / (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, 1971), by Air Force Flight Dynamics Laboratory (U.S.), H. A. Wood, Air Force Materials Laboratory (U.S.), and Fla.) Air Force Conference on Fatigue and Fracture of Aircraft Structures and Materials (1969 : Miami Beach (page images at HathiTrust)
• Fracture and fatigue strength evaluation of multiple site damaged aircraft fuselages : curved panel testing and analysis / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1994]), by G. Samavedam, D. Hoadley, Foster-Miller, John A. Volpe National Transportation Systems Center (U.S.), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Proceedings of the FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures : FAA Center of Excellence in Computational Modeling of Aircraft Structures, Atlanta, Georgia, August 28-30, 1996. (Washington, D.C. : Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by Ga.) FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures (1996 : Atlanta, Catherine Ann Bigelow, and National Aging Aircraft Research Program (U.S.) (page images at HathiTrust)
• Out-of-plane analysis for composite structures. (Warminster, PA : Naval Air Warfare Center, Aircraft Division, [1994]), by Philip C. Paul, Northrop Corporation. Aircraft Division, Naval Air Warfare Center (U.S.). Aircraft Division, and McDonnell Aircraft Corporation (page images at HathiTrust)
• Certification methodology for stiffener terminations / (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by C. H. Shah, M. Mahler, H. P. Kan, Northrop Corporation. Military Aircraft Division, Langley Research Center, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Automated inspection of aircraft / (Washington, D.C. : U.S. Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by C. J. Alberts, Carnegie-Mellon Institute of Research, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Homing performance comparison of selected airframe configurations using skid-to-turn and bank-to-turn steering policies / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by R. T. Reichert, Johns Hopkins University, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• The effect of aircraft size on cabin floor dynamic pulses / (Atlantic City Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1990]), by Gil Wittlin, Lockheed Aeronautical Systems Company, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Supplemental inspection document development program for the Cessna Model 402 / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1999]), by Larry Chan, Cessna Aircraft Company, United States Federal Aviation Administration, and United States. Office of Aviation Research (page images at HathiTrust)
• Development of a D sight aircraft inspection system, Phase II / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by F. Karpala, O. L. Hageniers, Diffracto Limited, Transportation Development Centre (Canada), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Characterization of corrosion and development of a breadboard model of a D sight aircraft inspection system, Phase I / (Atlantic City, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1994]), by F. Karpala, O. L. Hageniers, Diffracto Limited, Transportation Development Centre (Canada), and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Literature review and preliminary studies of fretting and fretting fatigue including special applications to aircraft joints / (Atlantic City Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1994]), by David Hoeppner, Mark W. Moesser, Saeed Adibnazari, University of Utah. Department of Mechanical Engineering, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Effects of repair on structural integrity / (Atlantic City International Airport : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1993]), by R. Rice, John A. Volpe National Transportation Systems Center (U.S.), Battelle Memorial Institute, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Generation of spectra and stress histories for fatigue and damage tolerance analysis of fuselage repairs / (Atlantic City, N.J. : FAA Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1991]), by David Broek, Richard C. Rice, Samuel H. Smith, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Fracture testing of large-scale thin-sheet aluminum alloy / (Washington, DC : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by R. DeWit, National Institute of Standards and Technology (U.S.). Metallurgy Division, and United States. Office of Aviation Research (page images at HathiTrust)
• Investigation of fuselage structure subject to widespread fatigue damage / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1996]), by M. L. Gruber, Boeing Company. Commercial Airplane Group, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Development of alternating current potential drop (ACPD) procedures for crack detection in aluminum aircraft panels / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1993]), by D. A. Jablonski, John A. Volpe National Transportation Systems Center (U.S.), Instron Corporation, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• A laboratory study of multiple site damage in fuselage lap splices / (Atlantic City International Airport, N.J. : Federal Aviation Administration Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1993]), by R. Mayville, M. Sigelmann, John A. Volpe National Transportation Systems Center (U.S.), Inc Arthur D. Little, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Longitudinal acceleration tests of overhead luggage bins and auxiliary fuel tank in a transport airplane airframe / (Washington, D.C.: Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1999]), by Robert J. McGuire, Tim Macy, Inc Transportation Research Center, William J. Hughes Technical Center (U.S.), and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Handbook : manufacturing advanced composite components for airframes / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by Terry L. Price, Cerritos College. Composites Training Ccenter, and United States. Federal Aviation Administration. Office of Aviation Research (page images at HathiTrust)
• Residual strength test on stiffened panels with multiple-site damage / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1999]), by H. J. ten Hoeve, Nationaal Lucht- en Ruimtevaartlaboratorium (Netherlands), and United States Federal Aviation Administration (page images at HathiTrust)
• Damage tolerance assessment handbook / (Atlantic City [International] Airport, NJ : FAA Technical Center ; Springfield, Va. : Available through the National Technical Information Service, [1993]), by John A. Volpe National Transportation Systems Center (U.S.) and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Video landing parameter survey, John F. Kennedy International Airport / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1997]), by Thomas DeFiore, Terrence Barnes, Richard Micklos, Federal Aviation Administration Technical Center (U.S.), Naval Air Warfare Center (U.S.), and United States. Office of Aviation Research (page images at HathiTrust)
• An analysis of ground-flight loads measured on the instrumented B-727 N40 / (Washington, D.C. : Federal Aviation Administration, Office of Aviation Research ; Springfield, Va. : Available through the National Technical Information Service, [1995]), by William M. Cavage, Terence Barnes, Tom DeFiore, Federal Aviation Administration Technical Center (U.S.), Galaxy Scientific Corporation, and United States. Office of Aviation Research (page images at HathiTrust)
• Fundamentals of [aircraft and missile] structures / ([Los Angeles] : Air Science Associates of Southern California for the U. S. Air Force Institute of Technology, Wright-Patterson Air Force Base, 1960), by Hugh Harrison Hurt (page images at HathiTrust)
• Proceedings of the International Conference on Aging Airplanes, June 1-3, 1988 / ([Washington, D.C.] : Federal Aviation Administration, [1989]), by Va.) International Conference on Aging Airplanes (1988 : Arlington, John A. Volpe National Transportation Systems Center (U.S.), and United States Federal Aviation Administration (page images at HathiTrust)
• Structural efficiency of aluminum multiweb beams and z-stiffened panels reinforced with filamentary boron-epoxy composite / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 20230], 1970), by James P. Peterson, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Investigation of fatigue-crack growth under simple variable-amplitude loading / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by C. M. Hudson, K. N. Raju, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Summary of center-of-gravity accelerations experienced by commercial transport airplanes in landing impact and ground operations / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1971), by Paul A. Hunter, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Response of a cantilever beam to non-stationary and stationary random excitation ([Wright-Patterson Air Force Base, Ohio, Air Force Materials Laboratory, Air Force Systems Command, 1968]), by P. Y. Wang and Masanobu Shinozuka (page images at HathiTrust)
• Experimenmtal flutter results for corrugation-stiffened and unstiffened panels / (Washington, D.C. : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, [1966]), by Deene J. Weidman and Langley Research Center (page images at HathiTrust)
• Experimental evaluation of nacelle-airframe interference forces and pressures at Mach numbers of 0.9 to 1.4 / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Daniel P. Bencze, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by Robert F. O'Connell, N. A. Radovcich, H. J. Hassig, Lockheed-California Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Derivation of a tapered p-version beam finite element / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ; Springfield, Va. : For sale by the National Technical Information Service, 1989), by Howard E. Hinnant and Langley Research Center. Aerostructures Directorate (page images at HathiTrust)
• Acoustic measurements of a large cavity in a wind tunnel / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), by James Scheiman and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Progress in supersonic cruise aircraft technology / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Office, 1978), by Cornelius Driver and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Aerodynamic characteristics of a high-wing transport configuration with an over-the-wing Nacelle-pylon arrangement / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1985), by William P. Henderson, William Kelly Abeyounis, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Rapid estimation of frequency response functions by close-range photogrammetry / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by John S. Tripp and Langley Research Center (page images at HathiTrust)
• A cracked orthotropic sheet stiffened by a semi-infinite orthotropic sheet / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1985), by C. A. Bigelow and Langley Research Center (page images at HathiTrust)
• Experimental and analytical study of an inlet forebody for an airframe-integrated scramjet concept / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Earl H. Andrews, S. Z. Pinckney, Anthony M. Agnone, and Langley Research Center (page images at HathiTrust)
• Effect of service usage on tensile, fatigue, and fracture properties of 7075-T6 and 7178-T6 aluminum alloys / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1975), by Richard A. Everett and Langley Research Center (page images at HathiTrust)
• Analysis of the space shuttle orbiter skin panels under simulated hydrodynamic loads / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Division : Springfield, Va. : For sale by the National Technical Information Service, 1988), by Huey D. Carden, Lisa E. Jones, and Edwin L. Fasanella (page images at HathiTrust)
• An integrated computer procedure for sizing composite airframe structures / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Jaroslaw Sobieszczanski-Sobieski, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Brazed Borsic/aluminum structural panels / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1977), by Thomas T. Bales, Dick M. Royster, H. Ross Wiant, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Airframe noise of a small model transport aircraft and scaling effects / (Washington, D.C. : U.S. National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by John G. Shearin, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Determination of airplane model structure from flight data using splines and stepwise regression / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Vladislav Klein, James G. Batterson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Internal convective cooling systems for hypersonic aircraft / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service, 1975]), by Frank M. Anthony, Robert G. Helenbrook, W. H. Dukes, Langley Research Center, and Bell Aerospace Textron (page images at HathiTrust)
• XB-70 structural mode control system design and performance analyses / (Washington, D.C. : National Aeronautics and Space Administration, 1970), by John H. Wykes, Alva S. Mori, Louis U. Nardi, United States National Aeronautics and Space Administration, Flight Research Center (U.S.), and North American Rockwell Corporation (page images at HathiTrust)
• Validation of scramjet exhaust simulation technique at Mach 6 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979), by H. B. Hopkins, J. Leng, W. Konopka, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Airframe noise of the DC-9-31 / (Washington : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by A. B. Bauer, Albert G. Munson, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Coupled rotor/airframe vibration analysis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Robert Sopher, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, United Technologies Corporation. Sikorsky Aircraft Division, Army Research and Technology Laboratories (U.S.). Structures Laboratory, and Langley Research Center (page images at HathiTrust)
• Service evaluation of aluminum brazed titanium (ABTi) / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1981), by S. D. Elrod, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Axial-load fatigue tests using loading schedules based on maneuver-load statistics. Eugene C. Naumann and Russell L. Schott. (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1962]), by Eugene C. Naumann, Russell L. Schott, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Landing approach airframe noise measurement and analysis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Paul L. Lasagna, Hugh L. Dryden Flight Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Full-scale crash-test evaluation of two load-limiting subfloors for general aviation airframes / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; Springfield, Va. : For sale by the National Technical Information Service, 1984), by Huey D. Carden and Langley Research Center (page images at HathiTrust)
• Validation of an active gear, flexible aircraft take-off and landing analysis (AGFATL) [microform] / (Hampton, Va. : Langley Research Center, 1984), by John R. McGehee and Langley Research Center (page images at HathiTrust)
• Validation of scramjet exhaust simulation technique / (Washington : National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by H. B. Hopkins, J. Leng, H. B. Konopka, United States National Aeronautics and Space Administration, Langley Research Center, and Grumman Aerospace Corporation (page images at HathiTrust)
• Study of a fail-safe abort system for an actively cooled hypersonic aircraft : volume I--technical summary / (Washington : U.S. National Aeronautics and Space Administration ; Springfield, Va. : For sale by the National Technical Information Service, 1976), by C. J. Pirrello, R. L. Herring, United States National Aeronautics and Space Administration, McDonnell Douglas Corporation, and Langley Research Center (page images at HathiTrust)
• Acceleration of fatigue tests for built-up titanium components / (Washington : U.S. National Aeronautics and Space Administration ; Springfield Va. : For sale by the National Technical Information Service, 1976), by R. T. Watanabe, United States National Aeronautics and Space Administration, Boeing Company, and Langley Research Center (page images at HathiTrust)
• Thermal design for areas of interference heating on actively cooled hypersonic aircraft / (Washington : National Aeronautics and Space Administration, Scientific and Technical Office ; Springfield, Va. : For sale by the National Technical Information Service, 1978), by R. L. Herring, J. E. Stone, McDonnell Douglas Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Statistical summaries of fatigue data for design purposes / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1983), by Paul H. Wirsching, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, Lewis Research Center, and University of Arizona (page images at HathiTrust)
• An analysis of aerodynamic requirements for coordinated bank-to-turn autopilots / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by A. Arrow, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Johns Hopkins University. Applied Physics Laboratory (page images at HathiTrust)
• Integrated airframe propulsion control / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1982), by Robert E. Fennell, Stephen B. Black, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Airframe noise component interaction studies / ([Washington] : National Aeronautics and Space Administration, Scientific and Technical Information Office ; Springfield, Va. : For sale by the National Technical Information Service, 1979), by Martin R. Fink, Robert H. Schlinker, United Technologies Research Center, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Dual methods and approximation concepts in structural synthesis / (Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [Springfield, Va. : For sale by the National Technical Information Service], 1980), by Claude Fleury, Lucien André Schmit, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• A method for the analysis of nonlinearities in aircraft dynamic response to atmospheric turbulence. (Washington : National Aeronautics and Space Administration ;, Springfield, Va. :, 1976), by Kenneth Sidwell (page images at HathiTrust)
• Influence of salt and elevated-temperature exposure on the maximum compressive strength of titanium-alloy skin-stringer panels / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the Clearinghouse for Federal Scientific and Technical Information, 1970]), by James E. Gardner, Dick M. Royster, and Langley Research Center (page images at HathiTrust)
• Cross-sectional deformations of monocoque beams and their side effects on the natural vibration frequencies / (Washington, [D.C.] : National Aeronautics and Space Administration, 1961), by Robert G. Thomson, Edwin T. Kruszewski, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Compressive behavior of titanium alloy skin-stiffener specimens selectively reinforced with boron-aluminum composite / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1971]), by Harvey W. Herring, Rosa C. Webster, Robert L. Carri, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Flight investigation of XB-70 structural response to oscillatory aerodynamic shaker excitation and correlation with analytical results [electronic resource] / (Washington, D.C. : National Aeronautics and Space Administration ; [Springfield, Va. : For sale by the National Technical Information Service], 1973), by James M. McKay, John H. Wykes, Eldon E. Kordes, United States National Aeronautics and Space Administration, and Flight Research Center (U.S.) (page images at HathiTrust)
• Noise response of cavities of varying dimensions at subsonic speeds / (Washington : National Aeronautics and Space Administration : Springfield, Va. : For sale by the National Technical Information Service, 1976), by Patricia J. W. Block and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Computational methods for structural mechanics and dynamics : proceedings of a workshop sponsored by the National Aeronautics and Space Administration and held at NASA Langley Research Center, Hampton, Virginia, June 19-21, 1985 / (Washington, D.C. : National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989), by W. Jefferson Stroud, Langley Research Center, and Workshop on Computational Methods for Structural Mechanics and Dynamics (1985 : NASA Langley Research Center) (page images at HathiTrust)
• Modal density estimates for sandwich panels : theory and experiment / (Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Clearinghouse for Federal Scientific and Technical, Springfield, Virginia 22151], 1970), by Larry L. Erickson, Ames Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust; US access only)
• Plane-stress analysis of an edge-stiffened rectangular plate subjected to boundary loads, boundary displacements, and temperature gradients / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by Chuan-jui Lin and Charles Libove (page images at HathiTrust; US access only)
• Fatigue behavior of a fusion welded ti-8Al-1Mo-1V simulated wing structure under the environment of a supersonic transport / (Washington, D.C. : National Aeronautics and Space Administration, 1967), by John J. Peterson (page images at HathiTrust; US access only)
• Airplane structures / (New York : Wiley, 1929), by Alfred Salem Niles (page images at HathiTrust)
• Airframe and powerplant mechanics : airframe handbook. ([Washington] : Dept. of Transportation, Federal Aviation Administration, Flight Standards Service : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1976), by United States. Flight Standards Service (page images at HathiTrust)
• Airframe and powerplant mechanics certification guide / (Washington : FAA : for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1976), by United States. Flight Standards Service (page images at HathiTrust)
• Airframe and powerplant mechanics certification guide. Rev. (Washington, Federal Aviation Administration; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1973), by United States. Flight Standards Service (page images at HathiTrust; US access only)
• Torsional instabilities in composite and composite-reinforced aluminum-alloy thin-walled cylinders / ([Washington : For sale by the Supt. of Docs., U.S. Govt. Print. Off.], 1972), by Donald E. Marlowe (page images at HathiTrust)
• Intermittent stressing and heating tests of aircraft structural metals /, by John Salvaggi, sponsor United States. Air Force. Air Research and Development Command, issuing body Wright Air Development Center, sponsor Aerospace Medical Laboratory (U.S.), and sponsor Cornell Aeronautical Laboratory (page images at HathiTrust)
• Determination of the mechanical properties of aircraft-structural materials at very high temperatures after rapid heating /, by James B. Preston, J. Robert Kattus, William P. Roe, United States. Air Force. Air Research and Development Command. sponsor, Southern Research Institute, and Wright Air Development Center (page images at HathiTrust)
• Investigation of the fatigue strength of a full-scale airplane wing structures / (Washington, D.C. : National Advisory Committee for Aeronautics, 1951), by Dwight O. Fearnow, Langley Aeronautical Laboratory, and United States. National Adviosry Committee for Aeronautics. NACA research memorandum (page images at HathiTrust)
• Report on material properties for design of airframe structures to operate at high temperatures /, by L. R. Jackson and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Solutions for hydrodynamic impact force and response of a two-mass system with an application to an elastic airframe / (Washington, D.C. : National Advisory Committee for Aeronautics, 1947), by Wilbur L. Mayo and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• An investigation of the stability of a system composed of a subsonic canard airframe and a canted-axis gyroscope automatic pilot / (Washington, D.C. : National Advisory Committee for Aeronautics, 1950), by Robert A. Gardiner, H. O. Ankenbruck, Jacob Zarovsky, and United States. National Advisory Committee for Aeronautics (page images at HathiTrust)
• Beryllium for structural applications : a review of the unclassified liturature / (Columbus, Ohio : Defense Metals Information Center, Battelle Memorial Institute, 1958), by Webster Hodge and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• A Review of certain ferrous castings applications in aircraft and missiles /, by John. Varga and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Report on the selection of materials for high-temperature applications in airframes /, by S. A. Gordon and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Supplement to TML Report No. 13 on the selection of materials for high-temperature applications in airframes /, by S. A. Gordon, L. R. Jackson, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Report on survey of experimental facilities for rolling thin, wide, high-strength, high-temperature materials for aircraft construction /, by R. L. Carlson, C. H. Lorig, and Defense Metals Information Center (U.S.) issuing body (page images at HathiTrust)
• Determination of the mechanical properties of aircraft-structural materials at very high temperatures after rapid heating : the effect of simultaneous heating and loading on the tensile properties of typical structural alloys /, by A. Clyde Willhelm, J. Robert Kattus, United States. Air Force. Air Research and Development Command. sponsor, Wright Air Development Center issuing body, Southern Research Institute, and Wright Air Development Center (page images at HathiTrust; US access only)
• A Koiter-type method for finite element analysis of nonlinear structural behavior. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by Raphael T. Haftka, W. Nachbar, R. H. Mallett, San Diego University of California, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Cracks, a Fortran IV digital computer program for crack propagation analysis /, by Robert M. Engle, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Elasto-plastic analysis of structures under load and two-dimensional temperature distributions., by P. C. Huang, R. J. Edwards, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.) sponsor, and sponsor Martin Marietta Corporation. Baltimore Division (page images at HathiTrust)
• Topics on flexible airplane dynamics /, by Julian Wolkovitch, R.K. Siskind, H.R. Pass, B. F. Pearce, United States. Air Force. Systems Command. Aeronautical Systems Division. issuing agency, sponsor Air Force Flight Dynamics Laboratory (U.S.), Inc Systems Technology, Wright-Patterson Air Force Base (Ohio), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Durability methods development., by S. D. Manning, Y. N. Kim, W. R. Garver, M. A. Flanders, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation (page images at HathiTrust)
• Durability methods development., by B. J. Pendley, S. D. Manning, S. P. Henslee, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation (page images at HathiTrust)
• A-10 static structural test program /, by Thomas F. Hughes, Frederick E. Hussong, Martin D. Richardson, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Flaw growth in complex structure., by Thomas R. Brussat, M. Creager, S. T. Chiu, issuing body United States. Air Force. Systems Command, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Del West Engineering, and sponsor Lockheed-California Company (page images at HathiTrust)
• Close tolerance steel forging development /, by C. E. Proffitt, H. C. Thomas, sponsor Boeing Company. Wichita Division, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Fracture mechanics of tiny cracks near fasteners /, by William E. Anderson, sponsor Battelle Memorial Institute. Columbus Laboratories, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• A Koiter-type method for finite element analysis of nonlinear structural behavior. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970), by Raphael T. Haftka, W. Nachbar, R. H. Mallett, San Diego University of California, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Durability methods development., by Masanobu Shinozuka, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Modern Analysis Inc. (page images at HathiTrust)
• Program for the development of extruded beryllium shapes /, by L. M. Christensen, R. R. Wells, sponsor Northrop Corporation, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Flaw growth in complex structure., by Thomas R. Brussat, M. Creager, S. T. Chiu, issuing body United States. Air Force. Systems Command, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Del West Engineering, and sponsor Lockheed-California Company (page images at HathiTrust)
• Handbook of force management methods /, by A. P. Berens, D. J. White, C. E. Larson, R. L. Johnson, J. C. Davis, K. E. Brown, D. S. Morcock, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Air Force Wright Aeronautical Laboratories, sponsor Vought Corporation, sponsor Lockheed-Georgia Company, and sponsor University of Dayton. Research Institute (page images at HathiTrust)
• Durability methods development., by J. N. Yang, W. R. Garver, S. D. Manning, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor General Dynamics Corporation, and sponsor George Washington University (page images at HathiTrust)
• Flaw growth in complex structure., by Thomas R. Brussat, M. Creager, S. T. Chiu, issuing body United States. Air Force. Systems Command, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Del West Engineering, and sponsor Lockheed-California Company (page images at HathiTrust)
• An automated procedure for computing the three-dimensional transonic flow over wing-body combinations, including viscous effects., by William H. Mason, Juanita Frick, W. F. Ballhaus, Mark Stern, Donald Mackenzie, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Grumman Aerospace Corporation, and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• An automated procedure for the optimization of practical aerospace structures. (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971), by Walter J. Dwyer, Patricia L. Sabatelli, Robert K. Emerton, sponsor Air Force Flight Dynamics Laboratory (U.S.), issuing body United States. Air Force. Systems Command, and sponsor Grumman Aerospace Corporation (page images at HathiTrust)
• Design and purchase expectations for fracture Resistance of 7000-series aluminum airframe alloys /, by William E. Anderson, sponsor Battelle Memorial Institute. Columbus Laboratories, and issuing body United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Digital load control applied to full-scale airframe fatigue tests /, by Nirmal K. Mondol, Richard M. Potter, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Modal investigation of lightweight aircraft structures using digital techniques /, by Robert W. Gordon, Richard D. Talmadge, H. F. Wolfe, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• Including fleet usage variability in reliability analyses for both safety and economic limit /, by Robert L. Neulieb, sponsor Air Force Flight Dynamics Laboratory (U.S.), and issuing body United States. Air Force. Systems Command (page images at HathiTrust)
• An analysis of flexible aircraft structural mode control., by John H. Wykes, Alva S. Mori, sponsor Wright-Patterson Air Force Base (Ohio), sponsor Air Force Flight Dynamics Laboratory (U.S.), and sposnor North American Aviation (page images at HathiTrust)
• The analytical determination of the thermal response of a typical aircraft structure subjected to transient external heating and cooling /, by Thomas N. Bernstein, Robert M. Engle, Gene E. Maddux, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• FORMAT II - Second version of Fortran matrix abstraction technique., by R. C. Morris, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• Fracture mechanics analysis of single and double rows of fastener holes loaded in bearing /, by Oscar Orringer, George Stalk, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, D. A. Tappeiner, T. E. Charbonneau, D. K. Hill, R. D. Grennan, R. A. Fox, D. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• The effect of various missile characteristics on airframe frequency response / (Washington, D.C. : National Advisory Committee for Aeronautics, [1952]), by Howard F. Matthews, Walter E. McNeill, United States. National Advisory Committee for Aeronautics. NACA research memorandum, and Ames Research Center (page images at HathiTrust)
• Tensile properties of aircraft-structural metals at various rates of loading after rapid heating /, by Joseph D. Morrison, J. R. Kattus, issuing body Wright Air Development Center, sponsor United States. Air Force. Air Research and Development Command, and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
• Integrated airframe - nozzle performance for designing twin-engine fighters., by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor Lockheed-California Company (page images at HathiTrust)
• Aeroelasticity in stability and control /, by United States. Department of the Air Force. Wright Air Development Center, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• Prediction of creep effects in aircraft structures /, by C. W. Alesch, W. Robe, W. H. Steurer, C. Riparbelli, sponsor United States. Wright Air Development Division, United States. Air Force. Air Research and Development Command. issuing body, and sponsor General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Low frequency instabilities of free systems /, by Robert G. Schwendler, Jack H. Hill, Computer Engineering Associates. sponsor, sponsor Air Force Flight Dynamics Laboratory (U.S.), sponsor Wright-Patterson Air Force Base (Ohio), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• The evaluation of acoustic impact technique for detection of incipients cracks in aircraft components., by Boeing Vertol Company and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Development of procedures for large scale automated minimum weight structural design /, by Ronald A. Gellatly, sponsor Bell Aerospace Textron, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Nondestructive holographic techniques for structures inspection /, by Robert K. Erf, H. G. Aas, K. A. Stetson, R. M. Gagosz, J. P. Waters, issuing agency Air Force Materials Laboratory (U.S.), and sponsor United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Sonic fatigue design techniques for advanced composite aircraft structures : Final report /, by Ian Holehouse, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and Inc. Rohr Industries (page images at HathiTrust)
• Establishment of the approach to, and development of, interim design criteria for sonic fatigue /, by G. E. Fitch, P. A. Clawson, P. Wang, P. M. Belcher, A. G. Tipton, L. M. Brennan, T. R. Dutko, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor North American Aviation (page images at HathiTrust)
• Manufacturing technology for Advanced Metal Removal Initiatives (AMRI)., by D. G. Flom, sponsor Air Force Wright Aeronautical Laboratories, and sponsor General Electric Company. Research and Development Center (page images at HathiTrust)
• Nondestructive holographic techniques for structures inspection /, by Robert K. Erf, G. Whitnery, F. Michael, R. M. Gagosz, J. P. Waters, issuing agency Air Force Materials Laboratory (U.S.), and sponsor United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• Parametric fatigue analysis of USAF aircraft /, by George J. Roth, James C. Sliemers, John P. Ryan, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Dayton. Research Institute (page images at HathiTrust)
• Nondestructive holographic techniques for structures inspection /, by Robert K. Erf, H. G. Aas, G. Whitnery, K. A. Stetson, R. M. Gagosz, J. P. Waters, issuing agency Air Force Materials Laboratory (U.S.), and sponsor United Aircraft Corporation. Research Laboratories (page images at HathiTrust)
• The minimum weight design of structures operating in an aerospace environment /, by H. Switzky, sponsor United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Republic Aviation Corporation (page images at HathiTrust)
• A crack growth gage for assessing flaw growth potential in structural components /, by R. L. Crane, J. P. Gallagher, A. F. Grandt, and issuing agency Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Fracture control procedures for aircraft structural integrity /, by Howard A. Wood and issuing agency Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Analytical design methods for aircraft structural joints /, by W. F. McCombs, J. L. Perry, J. C. McQueen, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor LTV Aerospace Corporation (page images at HathiTrust)
• Antifriction airframe bearing mounting study -90 to 2000 F /, by R. H. Bradley, J. W. Van Wyk, issuing agency United States. Air Force. Systems Command. Aeronautical Systems Division, and sponsor Boeing Company (page images at HathiTrust)
• Approximate multiple configuration analysis and allocation for least weight structural design /, by Robert J. Melosh, R. Luik, and issuing agency Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Optimality criteria in structural design /, by William Prager, Pedro V. Marcal, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Brown University. Division of Engineering (page images at HathiTrust)
• Design criteria for rolling element air frame bearings for high temperature and high altitude use /, by Harold E. Munson, J. H. Johnson, Jamshed B. Havewala, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Development of procedures for large scale automated minimum weight structural design /, by Ronald A. Gellatly, John A. Bruno, issuing agency Air Force Flight Dynamics Laboratory (U.S.), and sponsor Bell Aerospace Textron (page images at HathiTrust)
• The determination of lateral handling quality requirements from airframe-human pilot system studies /, by Irving L. Ashkenas, Duane T. McRuer, issuing body Wright Air Development Center, and sponsor United States. Air Force. Air Research and Development Command (page images at HathiTrust)
• The relationship of earliest failures to fleet size and "parent" population /, by Robert A. Heller, A. S. Heller, sponsor Air Force Materials Laboratory (U.S.), issuing agency United States. Air Force. Systems Command, and sponsor Columbia University. Department of Civil Engineering and Engineering Mechanics (page images at HathiTrust)
• A technique for obtaining improved real-time holographic interferometric data using pulse modulated illumination /, by Frank D. Adams, Gene E. Maddux, and issuing agency Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Response of nonlinear structural panels subjected to high intensity noise /, by C. Mei, issuing agency Air Force Wright Aeronautical Laboratories, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor University of Missouri--Rolla. Mechanical Engineering Department (page images at HathiTrust)
• Linearized dynamics of rotating aerospace vehicles with internal angular momenta /, by Duane T. McRuer, Julian Wolkovitch, United States. Air Force. Systems Command. Aeronautical Systems Division. sponsor, issuing agency United States. Air Force. Systems Command, Inc. Systems Technology, Inc Systems Technology, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• On the Reliability of redundant structures /, by Masanobu Shinozuka, Hiroshi Itagaki, sponsor Air Force Materials Laboratory (U.S.), issuing agency United States. Air Force. Systems Command, and sponsor Columbia University (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Hua Lin, Theodore H. H. Pian, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Gabriel Isakson, Claude Brenner, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body United States. Air Force. Air Matériel Command (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Theodore H. H. Pian, Hua Lin, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Hua Lin, Theodore H. H. Pian, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by F. O. Carta, Hua Lin, Theodore H. H. Pian, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Tensile properties of aircraft-structural metals at various rates of loading after rapid heating /, by J. R. Kattus, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and Ala.) Southern Research Institute (Birmingham (page images at HathiTrust)
• Heterogeneous construction for missile fuselages /, by Adam T. Zahorski, United States. Air Force. Air Research and Development Command. issuing body, Wright Air Development Center sponsor, and Inc. Zahorski Engineering (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by K. A. Foss, Theodore H. H. Pian, Sternlight D., sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by K. A. Foss, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by J. F. McCarthy, A. A. Kirsch, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by A. Codik, Theodore H. H. Pian, Hua Lin, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by A. A. Kirsch, J. F. McCarthy, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Hua Lin, Theodore H. H. Pian, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by S. J. Engel, J. F. McCarthy, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Prediction of creep effects in aircraft structures., by C. W. Alesch, W. Robe, B. Klein, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division, sponsor Air Force Flight Dynamics Laboratory (U.S.), and sponsor General Dynamics Corporation. Convair Division (page images at HathiTrust)
• Thermo-structural analysis manual., by Marvin J. Forray, M. Newman, H. Switzky, issuing body United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processes, and sponsor Republic Aviation Corporation (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Theodore H. H. Pian, P. H. Winter, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• Preservation and utilization of finite element models of USAF aircraft structures /, by Warren C. Gibson, Gordon Negaard, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
• Development of a mathematical model for predicting the percentage fatigue life increase resulting from shot peened components., by Roger S. Simpson, issuing body Air Force Wright Aeronautical Laboratories, and sponsor Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• FORMAT II : Second version of Fortran matrix abstraction technique :, by J. E. Serpanos, issuing agency Air Force Materials Laboratory (U.S.), and sponsor Douglas Aircraft Company. Aircraft Division (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by John Pickard, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by J. P. Cogan, J. R. Wells, J. E. Serpanos, R. C. Morris, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by John Pickard, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by R. C. Morris, P. S. Yoon, J. R. Wells, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by R. C. Morris, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by John Pickard, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. sponsor (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Theodore H. H. Pian, Hua Lin, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body Wright Air Development Center (page images at HathiTrust)
• FORMAT : Fortran matrix abstraction technique., by J. A. Frank, Air Force Flight Dynamics Laboratory (U.S.). issuing body, Air Force Wright Aeronautical Laboratories. sponsor, and Douglas Aircraft Company. Aircraft Division. sponsor (page images at HathiTrust)
• Effect of structural flexibiligy on aircraft loading., by Gabriel Isakson, Norman P. Hobbs, sponsor Massachusetts Institute of Technology. Aeroelastic and Structures Research Laboratory, and issuing body United States. Air Force. Air Matériel Command (page images at HathiTrust)

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