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Boeing Commercial Airplane Company

Books from the extended shelves:

• Boeing Commercial Airplane Company: 4D-TECS integration for NASA TSRV airplane (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by I. Kaminer, P. R. O'Shaughnessy, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Aerodynamic design and analysis system for supersonic aircraft (National Aeronautics and Space Administration ;, 1975), also by W. D. Middleton, R. G. Coleman, J. L. Lundry, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Aerodynamic influence coefficient method using singularity splines (National Aeronautics and Space Administration ;, 1974), also by J. E. Mercer, E. P. Lesferd, J. A. Weber, and Ames Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Aircraft command in emergency situations (ACES) : Phase I, Concept development (Federal Aviation Administration Technical Center ;, 1991), also by Thomas L. Reynolds, Charles D. Anderson, Gregory E. Grimstad, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Boeing Commercial Airplane Company: Airplane tests of enhanced emergency smoke venting (Federal Aviation Administration Technical Center ;, 1989), also by Elliott L. Maylor and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Boeing Commercial Airplane Company: Analysis of sonic boom measurements near shock wave extremities for flight near Mach 1.0 and for airplane accelerations (National Aeronautics and Space Administration ;, 1974), also by George T. Haglund, Edward J. Kane, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Analytical and experimental investigation of aircraft metal structures reinforced with filamentary composites (National Aeronautics and Space Administration ;, 1971), also by S. Oken, Langley Research Center, Boeing Company, and Boeing Company. Commercial Airplane Group (page images at HathiTrust)
• Boeing Commercial Airplane Company: Analytical investigation of fan tone noise due to ingested atmospheric turbulence (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1980), also by Ulrich W. Ganz and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Comparison of wind-tunnel test results at M[subscript infinity] = 0.7 with results from the Boeing TEA-230 subsonic flow method (National Aeronautics and Space Administration ;, 1975), also by Larry Wayne Mohn and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Computation of the transonic perturbation flow fields around two- and three-dimensional oscillating wings (National Aeronautics and Space Administration ;, 1975), also by W. H. Weatherill, James D. Sebastian, F. Edward Ehlers, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Computation of transonic potential flow about three-dimensional inlets, ducts, and bodies (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by Theodore A. Reyhner, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Boeing Commercial Airplane Company: A computational system for aerodynamic design and analysis of supersonic aircraft : part 2, user's manual (National Aeronautics and Space Administration ;, 1976), also by W. D. Middleton, Robert Griffin Coleman, J. L. Lundry, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boeing Commercial Airplane Company: Coupling linearized far-field boundary conditions with nonlinear near-field solutions in transonic flow (Bolling Air Force Base, D. C. : Air Force Office of Scientific Research, United States Air Force, 1988., 1988), also by William Rowe, F. Edward Ehlers, and United States. Air Force. Office of Scientific Research (page images at HathiTrust)
• Boeing Commercial Airplane Company: Cyclic debonding of adhesive joints : summary report (National Aeronautics and Space Administration ;, 1973), also by Daniel J. Hoffman, R. R. June, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Descent strategy comparisons for TNAV-equipped aircraft under airplane-preferred operating conditions (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1989), also by K. H. Izumi and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Design of integrated pitch axis for autopilot/autothrottle and integrated lateral axis for autopilot/yaw damper for NASA TSRV airplane using integral LQG methodology (National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division ;, 1990), also by Isaac Kaminer and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Detection of cracks under installed fasteners (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory , Air Force Systems Command, United States Air Force, 1974, 1974), also by C. F. Raatz, W. E. Woodmansee, R. A. Senske, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Boeing Commercial Airplane Company: The development and evaluation of color systems for airborne applications : phase I, fundamental visual, perceptual, and display system considerations (Federal Aviation Administration, Program Engineering & Maintenance Service ;, 1985), also by Louis D. Silverstein, Robin M. Merrifield, General Physics Corporation, and United States. Federal Aviation Administration. Program Engineering & Maintenance Service (page images at HathiTrust)
• Boeing Commercial Airplane Company: Development of acoustically lined ejector technology for multitube jet noise suppressor nozzles by model and engine tests over a wide range of jet pressure ratios and temperatures (National Aeronautics and Space Administration ;, 1974), also by J. Atvars and Lewis Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Development of integrated programs for aerospace-vehicle design (IPAD), product program management systems (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by J. M. Isenberg, J. W. Southall, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Development of Integrated Programs for Aerospace-Vehicle Design (IPAD) : reference design process (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Donald D. Meyer and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Development of quality assurance methods for epoxy graphite prepreg (National Aeronautics and Space Adminstration, Scientific and Technical Information Branch ;, 1982), also by J. S. Chen, A. B. Hunter, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Drag measurements of upswept afterbodies and analytical study on axisymmetric separation (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, 1974., 1974), also by Mansop Hahn, Theodore C. Nark, Paul E. Rubbert, Gunter W. Brune, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Boeing Commercial Airplane Company: Effects of service environments on aluminum-brazed titanium (ABTi) (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by W. L. Cotton, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Elastic buckling analysis for composite stiffened panels and other structures subjected to biaxial inplane loads (National Aeronautics and Space Administration ;, 1973), also by A. V. Viswanathan, M. Tamekuni, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Elastic stability of laminated, flat and curved, long rectangular plates subjected to combined inplane loads (National Aeronautics and Space Administration ;, 1974), also by A. V. Viswanathan, L. L. Baker, M. Tamekuni, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Enhanced emergency smoke venting (Federal Aviation Administration Technical Center ;, 1988), also by Elliott L. Maylor and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Boeing Commercial Airplane Company: Experimental evaluation of a Mach 3.5 axisymmetric inlet (National Aeronautics and Space Administration ;, 1975), also by J. Syberg, J. L. Koncsek, and Ames Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: A finite difference method for the solution of the transonic flow around harmonically oscillating wings (National Aeronautics and Space Administration ;, 1974), also by F. Edward Ehlers and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Flight effects on noise generated by the JT8D engine with inverted primary/fan flow as measured in the NASA-Ames 40- by 80-foot wind tunnel (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Frank G. Strout and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Flight phase status monitor study : phase I, systems concepts (Federal Aviation Administration, Program Engineering and Maintenance Service ;, 1984), also by L. G. Summers, Lockheed Aircraft Corporation, Douglas Aircraft Company, and United States. Federal Aviation Administration. Program Engineering & Maintenance Service (page images at HathiTrust)
• Boeing Commercial Airplane Company: A harmonic analysis method for unsteady transonic flow and its application to the flutter of airfoils (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), also by F. Edward Ehlers, W. H. Weatherill, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: High-transonic-speed transport aircraft study : summary report (National Aeronautics and Space Administration ;, 1974), also by Robert M. Kulfan and Ames Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Integrated application of active controls (IACC) technology to an advanced subsonic transport : project plan (National Aeronautics and Space Admininstration, Scientific and Technical Information Branch ;, 1981), also by Langley Research Center and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Boeing Commercial Airplane Company: Investigation of refracting flows for acoustic suppression (National Aeronautics and Space Administration ;, 1977), also by Denis Sloan, Bannister W. Farquhar, Robert B. Purves, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boeing Commercial Airplane Company: Measurements and predictions of flyover and static noise of a TF30 afterburning turgofan engine (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Frank W. Burcham, Stanley C. Oas, Paul L. Lasagna, Hugh L. Dryden Flight Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: A method for computing the leading-edge suction in a higher-order panel method (National Aeronautical and Space Administration, Scientific and Technical Information Office ;, 1984), also by F. Edward Ehlers, Marjorie E. Manro, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Operational analysis of time-frequency collision avoidance systems (Boeing Company, Commercial Airplane Division, 1968), also by Alex S. L. Nagy (page images at HathiTrust)
• Boeing Commercial Airplane Company: The practical application of a finite difference method for analyzing transonic flow over oscillating airfoils and wings (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by F. Edward Ehlers, James D. Sebastian, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Prediction of unsteady aerodynamic loadings caused by leading edge and trailing edge control surface motions in subsonic compressible flow : analysis and results (National Aeronautics and Space Administration ;, 1975), also by W. S. Rowe and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: A program to compute three-dimensional subsonic unsteady aerodynamic characteristics using the doublet lattice method, L216 (DUBFLEX) (National Aeronautics and Space Administration ;, 1979), also by M. Richard, B. A. Harrison, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Reduction of acoustic disturbances in the test section of supersonic wind tunnels by laminarizing their nozzle and test section wall boundary layers by means of suction (National Aeronautics and Space Administration ;, 1974), also by W. Pfenninger, J. Syberg, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Study of advanced composite structural design concepts for an arrow wing supersonic cruise configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by M. J. Turner, D. L. Grande, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Study of metallic structural design concepts for an arrow wing supersonic cruise configuration (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1977), also by M. J. Turner, D. L. Grande, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Boeing Commercial Airplane Company: Study of supersonic wings employing the attainable leading-edge thrust concept (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by W. D. Middleton, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Three-dimensional transonic potential flow about complex three-dimensional configurations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1984), also by Theodore A. Reyhner, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Traffic Alert and Collision Avoidance System : developmental simulation (Federal Aviation Administration, Program Engineering & Maintenance Service ;, 1982), also by G. P. Boucek and United States. Federal Aviation Administration. Program Engineering & Maintenance Service (page images at HathiTrust)
• Boeing Commercial Airplane Company: Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuaration / summary report (National Aeronautics and Space Administration ;, 1977), also by Marjorie E. Manro and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Boeing Commercial Airplane Company: Transonic pressure measurements and comparison of theory to experiment for an arrow-wing configuration (National Aeronautics and Space Administration ;, 1976), also by Marjorie E. Manro and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: Upper-surface blowing nacelle design study for a swept wing airplane at cruise conditions (National Aeronautics and Space Administration ;, 1974), also by W. B. Gillette and Langley Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: V/STOL lift fan commercial short-haul transports : continuing conceptual design study (National Aeronautics and Space Administration ;, 1974), also by J. M. Zabinsky and Ames Research Center (page images at HathiTrust)
• Boeing Commercial Airplane Company: YC-14 interior noise measurements program (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1981., 1981), also by L. M. Butzel, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)

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