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Lockheed-Georgia Company

Books from the extended shelves:

• Lockheed-Georgia Company: Analysis of a theoretically optimized transonic airfoil (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by M. E. Lores, George D. Shrewsbury, Kenneth P. Burdges, and Ames Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: An analysis of flight test data on the C-141A aircraft (National Aeronautics and Space Administration ;, 1970), also by J. H. Paterson and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Analytical sensor redundancy assessment (FAA Technical Center ;, 1988), also by D. B. Mulcare, M. K. Smith, L. E. Downing, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Application of a three-dimensional steady and unsteady full potential method for transonic flow computations (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1984, 1984), also by J. B. Malone, N. L. Sankar, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Application of active controls technology to the NASA JetStar airplane (National Aeronautics and Space Administration ;, 1975), also by R. H. Lange and Flight Research Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Applications of Compton backscatter radiation to nondestructive testing : final report (Lockheed-Georgia Company ;, 1961), also by John H. Tolan, K. E. Mears, C. T. Bradshaw, and U.S. Atomic Energy Commission. Savannah River Operations Office (page images at HathiTrust)
• Lockheed-Georgia Company: Argentine C-130 economic justification report : analysis of benefits and costs pertaining to the purchase and operation of right C-130 cargo aircraft by the Government of Argentina (Lockheed-Gerogia Company, 1962), also by K. M. Mayer and J. Ruys (page images at HathiTrust; US access only)
• Lockheed-Georgia Company: Basic experimental study of the coupling between flow instabilities and incident sound (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1984), also by K. K. Ahuja, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Calculation of unsteady transonic aerodynamics for oscillating wings with thickness (National Aeronautics and Space Administration ;, 1975), also by S. Y. Ruo, J. G. Theisen, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Cavity oscillation in cruise missile carrier aircraft (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 Harold W. Bartel, James M. McAvoy, Air Force Wright Aeronautical Laboratories, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Correlation of data related to shock-induced trailing-edge separation and extrapolation to flight Reynolds number (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1979), also by J. F. Cahill, P. C. Connor, and Ames Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Correlation of full-scale drag predictions with flight measurements on the C-141A aircraft : phase II, wind tunnel test, analysis, and prediction techniques (National Aeronautics and Space Administration ;, 1974), also by D. G. MacWilkinson, J. H. Paterson, W. T. Blackerby, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Determination of design data for heat treated titanium alloy sheet. Volume 1, Summary of mechanical and physical property data collected, including tensile creep and fatigue (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by P. J. Hughes and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-Georgia Company: Determination of design data for heat treated titanium alloy sheet. Volume 2a. Details of data collection program. Test techniques and results for tension, compression, bearing, shear, crippling, joints, and physical properties (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by W. M. McGee, B. R. Matthews, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-Georgia Company: Determination of design data for heat treated titanium alloy sheet. Volume 2b, Test techniques and results for creep and fatigue (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by D. L. White, H. T. Watson, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-Georgia Company: Determination of design data for heat treated titanium alloy sheet. Volume 3., Tables of data collected (Wright-Patterson Air Force Base, Ohio : Directorate of Materials and Processes, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-Georgia Company: Determination of moisture content in composites by dielectric measurements (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1979., 1979), also by A. O. Kays, Air Force Flight Dynamics Laboratory (U.S.), and Air Force Wright Aeronautical Laboratories (page images at HathiTrust)
• Lockheed-Georgia Company: Digital system bus integrity (Federal Aviation Administration Technical Center ;, 1987), also by Donald Eldredge, Ellis F. Hitt, Battelle Memorial Institute. Columbus Laboratories, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Effects of underloads on fatigue crack growth. Volume II, Data tabulations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1977., 1977), also by W. M. McGee, T. M. Hsu, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-Georgia Company: Evaluation of a reliability analysis approach to fatigue life variability of aircraft structures using C-130 in-dervice operational data (Wright-Patterson Air Force Base, Ohio : Air Force Materials Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Claude S. Sarphie, Robert S. Watson, and Air Force Materials Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Extended study of flaw growth at fastener holes. Volume 1 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by T. M. Hsu, J. A. Aberson, W. M. McGee, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-Georgia Company: Extended study of flaw growth at fastener holes. Volume 2, Data tabulation (Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978), also by T. M. Hsu, W. M. McGee, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Lockheed-Georgia Company: Finite element computer program to analyze cracked orthotropic sheets (U.S. National Aeronautics and Space Administration ;, 1976), also by C. S. Chu and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-Georgia Company: Flight text investigation of transonic shock-boundary layer phenomena (Wright-Patterson Air Force Base, Ohio : Air Force Systems Command, Air Force Flight Dynamics Laboratory, 1968., 1968), also by Jones F. Cahill, Bill L. Copper, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: The free jet as a simulator of forward velocity effects on jet noise (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by K. K. Ahuja, H. K. Tanna, B. J. Tester, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, and Lewis Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Group performance during four-hour periods of confinement (Wright-Patterson Air Force Base, Ohio : Behavioral Sciences Laboratory, 6570th Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, 1962., 1962), also by Earl A. Alluisi, W. Dean Chiles, Thomas J. Hall, and Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Handbook of force management methods (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 A. P. Berens, D. J. White, C. E. Larson, R. L. Johnson, J. C. Davis, K. E. Brown, D. S. Morcock, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, Vought Corporation, and University of Dayton. Research Institute (page images at HathiTrust)
• Lockheed-Georgia Company: Hardware fault insertion and instrumentation system : experimentation and results (FAA Technical Center ;, 1987), also by J. W. Benson, W. E. Larsen, Dennis B. Mulcare, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Hardware fault insertion and instrumentation system : mechanization and validation (FAA Technical Center ;, 1987), also by J. W. Benson and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: High Reynolds number test of a NACA 65₁-213, a = 0.5 airfoil at transonic speeds (National Aeronautics and Space Administration ;, 1975), also by Kenneth P. Burdges, Gerald A. Pounds, James A. Blackwell, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: High Reynolds number tests of a C141A aircraft semispan model to investigate shock-induced separation (National Aeronautics and Space Administration ;, 1975), also by W. T. Blackerby, J. F. Cahill, and Ames Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: High-speed flow past wings (National Aeronautics and Space Administration ;, 1973), also by Helge Nørstrud and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Human performance as a function of the work-rest ratio during prolonged confinement (Wright-Patterson Air Force Base, Ohio : Behavioral Sciences Laboratory, Aerospace Medical Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1961., 1961), also by Oscar S. Adams, W. Dean Chiles, Aerospace Medical Laboratory (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Lockheed-Georgia Company: Investigation of stress-strain history modeling at stress risers : Phase 2 (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1978., 1978), also by James R. Carroll, R. F. Wilkinson, R. L. Brugh, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: An investigation of the effects of surrounding structure on sonic fatigue (National Aeronautics and Space Administration, 1970), also by Thomas F. Nelson, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Mathematical model for two-dimensional multi-component airfoils in viscous flow (National Aeronautics and Space Administration, 1971), also by W. A. Stevens, J. A. Braden, and Suresh H. Goradia (page images at HathiTrust)
• Lockheed-Georgia Company: Model tests of jet-induced lift effects on a VTOL aircraft in hover (National Aeronautics and Space Administration ;, 1969), also by P. K. Shumpert, J. G. Tibbetts, Langley Research Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-Georgia Company: N-version software demonstration for digital flight controls (FAA Technical Center ;, 1987), also by Dennis B. Mulcare, Lynn A. Barton, and Federal Aviation Administration Technical Center (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: NASA CR-1845 (National Aeronautics and Space Administration ;, 1971), also by J. G. Hicks, J. F. Nash, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Noise characteristics of upper surface blown configurations : analytical studies (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Narayana N. Reddy, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Non-engine aerodynamic noise investigation of a large aircraft (National Aeronautics and Space Administration ;, 1974), also by J. S. Gibson and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Numerical aircraft design using 3-D transonic analysis with optimization. Volume 1, Executive summary (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 Andrew J. Srokowski, P. Aidala, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Grumman Aerospace Corporation (page images at HathiTrust)
• Lockheed-Georgia Company: Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Fighter design (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 P. Aidala, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Grumman Aerospace Corporation (page images at HathiTrust)
• Lockheed-Georgia Company: Numerical aircraft design using 3-D transonic analysis with optimization. Volume 2 Part 1, Transport design (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 Andrew J. Srokowski, P. R. Simth, R. A. Weed, M. E. Lores, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Grumman Aerospace Corporation (page images at HathiTrust)
• Lockheed-Georgia Company: Numerical aircraft design using 3-D transonic analysis with optimization. Volume 3 Part 1, User's guide to transport design computer programs (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 R. A. Weed, Andrew J. Srokowski, Air Force Flight Dynamics Laboratory (U.S.), Air Force Wright Aeronautical Laboratories, and Grumman Aerospace Corporation (page images at HathiTrust)
• Lockheed-Georgia Company: Performance and physiological effects of long term vibration (Wright-Patterson Air Force Base, Ohio : Aerospace Medical Research Laboratories, Aerospace Medical Division, Air Force Systems Command, United States Air Force, 1966., 1966), also by C. L. Holland and Aerospace Medical Research Laboratories (U.S.) (page images at HathiTrust)
• Lockheed-Georgia Company: Refinement and application of acoustic impulse technique to study nozzle transmission characteristics (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by M. Salikuddin, Lewis Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Lockheed-Georgia Company: Residual strength and crack propagation tests on C-130 airplane center wings with service-imposed fatigue damage (National Aeronautics and Space Administration ;, 1972), also by H. Lawrence Snider, William Dirkin, Franklin L. Reeder, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Steady flow ejector research program; final report for extended contract Nonr-3067(00) [by] J.K. Johnson, Jr., P.K. Shumpert [and] J.F. Sutton. ([Marietta, Ga.?], 1961), also by J. F. Sutton, P. K. Shumpert, and J. K. Johnson (page images at HathiTrust; US access only)
• Lockheed-Georgia Company: Stochastic disturbance data for flight control system analysis (Directorate of Aeromechanics, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962), also by John E. Hart, Larry L. Lacau, Lowry A. Adkins, United States. Air Force. Systems Command. Aeronautical Systems Division, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Lockheed-Georgia 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-California Company, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Lockheed-Georgia Company: Study of stability of large maneuvers of airplanes (National Aeronautics and Space Administration, 1974), also by Emile K. Haddad and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Theoretical and experimental study of a new method for prediction of profile drag of airfoil sections (National Aeronautics and Space Administration ;, 1975), also by Suresh H. Goradia, D. G. Lilley, and Langley Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Tone-excited jet : theory and experiments (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1982), also by K. K. Ahuja, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Lewis Research Center (page images at HathiTrust)
• Lockheed-Georgia Company: Wing pressure distribution and boundary layer data obtained from C-5A flight testing (Wright-Patterson Air Force Base, Ohio : Aerospace Research Laboratories, Air Force Systems Command, United States Air Force, 1974., 1974), also by Jones F. Cahill, William A. Stevens, and Aerospace Research Laboratories (U.S.) (page images at HathiTrust)

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