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Books about Lockheed-California Company -- Books by Lockheed-California Company

Books about Lockheed-California Company:

Books by Lockheed-California Company:

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• Lockheed-California Company: Advanced residual strength degradation rate modeling for advanced composite structures. Volume 1. Task I: Preliminary screening (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by D. E. Pettit, J. M. Cox, K. N. Lauraitis, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Advanced residual strength degradation rate Modeling for advanced composite structures. Volume 2. Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Advanced residual strength degradation rate modeling for advanced composite structures. Volume 3. Appendixes to report for Tasks II and III (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by K. N. Lauraitis, D. E. Pettit, J. T. Ryder, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Advanced supersonic technology concept study : hydrogen fueled configuration : summary report (National Aeronautics and Space Administration ;, 1975), also by G. Daniel Brewer, R. E. Morris, and Ames Research Center (page images at HathiTrust)
• Lockheed-California Company: Analytical modeling of transport aircraft crash scenarios to obtain floor pulses (Federal Aviation Administration, Systems Research and Development Service] ;, 1983), also by Dave Lackey, Gil Wittlin, Federal Aviation Administration Technical Center (U.S.), United States National Aeronautics and Space Administration, and United States. Federal Aviation Administration. Systems Research and Development Service (page images at HathiTrust)
• Lockheed-California Company: Commercial aircraft noise definition, L-1011 TriStar : final report (U.S. Dept. of Transportation, Federal Aviation Administration, Office of Environmental Quality, 1974), also by Nathan Shapiro and United States. Federal Aviation Administration. Office of Environmental Quality (page images at HathiTrust)
• Lockheed-California Company: Development design methods for predicting hypersonic aerodynamic control characteristics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by Z. Popinski, C. F. Ehrlich, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Development of advanced avionics systems applicable to terminal-configured vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by R. L. Heimbold, M. F. Leffler, H. P. Lee, and Langley Research Center (page images at HathiTrust)
• Lockheed-California Company: Effect of Mach number, Reynolds number, and thickness ratio on the aerodynamic characteristics of NACA 63A-series airfoil sections (Fort Eustis, Virginia : U.S. Army Aviation Materiel Laboratories, June 1965., 1965), also by O. E. Sipe, N. B. Gorenberg, and U.S. Army Aviation Materiel Laboratories (page images at HathiTrust)
• Lockheed-California Company: Effects of combined acoustic and flight loads on crack growth (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1976., 1976), also by J. Soovere, S. T. Chiu, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-California Company: Effects of nacelle configuration/position on performance of subsonic transport (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by L. H. Bangert, D. K. Krivec, R. N. Segall, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Lockheed-California Company: An Engineering evaluation of methods for the prediction of fatigue life in airframe structures (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Aeronautical Systems Division, AIr Force Systems Command, United States Air Force, 1962., 1962), also by W. J. Crichlow, M. A. Melcon, L. Young, A. J. McCulloch, United States. Air Force. Systems Command. Aeronautical Systems Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Evaluation of structural design concepts for an arrow-wing supersonic cruise aircraft (National Aeronautics and Space Administration ;, 1977), also by I. F. Sakata, G. W. Davis, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-California Company: Experimental and analytical determination of integrated airframe nozzle performance. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972, 1972), also by Edsel R. Glasgow, S. J. Smyth, R. F. Smith, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-California Company: Experimental and analytical determination of integrated airframe nozzle performance. Volume II, Operating manual for twin-nozzle/aftbody drag and internal nozzle performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Edsel R. Glasgow, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-California Company: An experimental and analytical investigation of hypersonic inlet boundary layers (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1965., 1965), also by J. F. Stroud, L. D. Miller, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Feasibility and tradeoffs of a transport fuselage fire management system: final report (1976) (page images at HathiTrust)
• Lockheed-California Company: Flaw growth in complex structure. Volume 1, Technical discussion (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Del West Engineering (page images at HathiTrust)
• Lockheed-California Company: Flaw growth in complex structure. Volume 2, Test data (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Del West Engineering (page images at HathiTrust)
• Lockheed-California Company: Flaw growth in complex structure. Volume 3, Summary, assessments, conclusions (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1977., 1977), also by Thomas R. Brussat, M. Creager, S. T. Chiu, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Del West Engineering (page images at HathiTrust)
• Lockheed-California Company: General aviation airplane structural crashworthiness programmer's manual : final report (U.S. Federal Aviation Administration Systems Research & Development Service, 1979), also by William L. LaBarge, United States. Federal Aviation Administration. Systems Research and Development Service, and Cessna Aircraft Company (page images at HathiTrust)
• Lockheed-California Company: A generalized vortex lattlice method for subsonic and supersonic flow applications (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by Luis R. Miranda, William M. Baker, Robert D. Elliott, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Lockheed-California Company: High altitude gust criteria for aircraft design (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1970., 1970), also by Edward V. Ashburn, Craig A. Melvin, David E. Waco, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-California Company: In-flight measurement and correlation with theory of blade airloads and responses on the XH-51A compound helicopter rotor (Fort Eustis, Virginia : U.S. Army Aviation Materiel Laboratories, 1968., 1968), also by U.S. Army Aviation Materiel Laboratories (page images at HathiTrust)
• Lockheed-California Company: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume I (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. K. Hill, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume II, Wind tunnel data identification and presentation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also 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, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume IV, Operating manual for subsonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume V, Operating manual for supersonic axisymmetric nozzle boattail drag computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, T. J. Jones, T. E. Charbonneau, Leonard D. Miller, Don M. Santman, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Integrated airframe - nozzle performance for designing twin-engine fighters. Volume VI, Revised operating manual for twin nozzle/afterbody drag and nozzle internal performance computer deck (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1973., 1973), also by Edsel R. Glasgow, D. A. Tappeiner, R. Posthumus, R. D. Grennan, R. A. Fox, Leonard D. Miller, Don M. Santman, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Investigation of mechanisms of potential aircraft fuel tank vent fires and explosions caused by atmospheric electricity (National Aeronautics and Space Administration :, 1964), also by United States. Federal Aviation Agency and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-California Company: Jimsphere wind and turbulence exceedance statistics (National Aeronautics and Space Administration ;, 1972), also by Stanley I. Adelfang, A. Court, and George C. Marshall Space Flight Center (page images at HathiTrust)
• Lockheed-California Company: LH2 Airport requirements study (U.S. National Aeronautics and Space Administration ;, 1976), also by United States National Aeronautics and Space Administration and Langley Research Center, ed. by G. D. Brewer (page images at HathiTrust)
• Lockheed-California Company: A literature survey of airborne vehicles impacting with water and soil : head injury criteria and severity index development of computer program KRASH (Federal Aviation Administration Technical Center ;, 1992), also by Gil Wittlin, Max A. Gamon, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Measurement and analysis of aircraft far-field aerodynamic noise (National Aeronautics and Space Administration ;, 1974), also by Gerald J. Healy and Langley Research Center (page images at HathiTrust)
• Lockheed-California Company: Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft. Part III, Aerodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by C. F. Ehrlich, C. M. Onspaugh, R. S. Peyton, J. J. Rising, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Preliminary design and experimental investigation of the FDL-5A unmanned high L/D spacecraft.. Part IV, Aerothermodynamics (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1968., 1968), also by F. L. Guard, H. D. Schultz, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-California Company: Proceedings of the ONR-NSIA Symposium on Automatic Collection, Processing and Analysis of Oceanographic Data : University of California, San Diego, 11-12 December 1964 (published for ONR and NSIA by the Lockheed-California Company, 1965), also by Processing and Analysis of Oceanographic Data Symposium on Automatic Collection, National Security Industrial Association, and United States. Office of Naval Research (page images at HathiTrust)
• Lockheed-California Company: Real-time testing of titanium sheet and extrusion coupon specimens subjected to Mach 2.7 supersonic cruise aircraft wing stresses and temperatures (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977), also by Tjerand Lunde and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Lockheed-California Company: Relative annoyance and loudness judgments of various simulated sonic boom waveforms (National Aeronautics and Space Administration ;, 1968), also by L. J. Shepherd, W. W. Sutherland, Langley Research Center, and Stanford Research Institute (page images at HathiTrust)
• Lockheed-California Company: Spectra of internal waves over basins and banks off Southern California (Lockheed-California Co., 1963), also by A. J Carsola, J. C Roque, and D. P Hamm (page images at HathiTrust)
• Lockheed-California Company: Study of flutter related computational procedures for minimum weight structural sizing of advanced aircraft (U.S. National Aeronautics and Space Administration ;, 1976), also by Robert F. O'Connell, N. A. Radovcich, H. J. Hassig, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-California Company: Study of quiet turbofan STOL aircraft for short haul transportation (National Aeronautics and Space Administration, 1973), also by T. P. Higgins, H. S. Sweet, E. G. Stout, Lockheed-Georgia Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-California Company: Study on the feasibility of V/STOL concepts for short haul transport aircraft (National Aeronautics and Space Administration, 1967) (page images at HathiTrust)
• Lockheed-California Company: Tests to determine subsonic aerodynamic characteristics of hypersonic re-entry configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by K. Mantz, R. Ross, D. B. Seager, Aeronautical Systems Center (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-California Company: Tests to determine subsonic pressures, forces and moments acting on a hypersonic re-entry configurations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by K. Mantz, R. Ross, D. B. Seager, United States. Air Force. Systems Command. Aeronautical Systems Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

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