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Books about Grumman Aerospace Corporation -- Books by Grumman Aerospace Corporation

Books about Grumman Aerospace Corporation:

Books by Grumman Aerospace Corporation:

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• Grumman Aerospace Corporation: Acoustic scattering by circular cylinders of various aspect ratios (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Algirdas Maciulaitis and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Grumman Aerospace Corporation: An algorithm for Liapunov stability analysis of complex nonlinear systems with application to the Orbiting Astronomical Observatory (National Aeronautics and Space Administration ;, 1971), also by Gunther R. Geiss and Ames Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Analysis of wing-body interaction flutter for a preliminary space shuttle design (National Aeronautics and Space Administration ;, 1974), also by Richard R. Chipman, Peter Shyprykevich, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Analysis of wing slipstream flow interaction (National Aeronautics and Space Administration, 1970), also by Antony Jameson, United States National Aeronautics and Space Administration, and Ames Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Analytical and experimental study of the effects of wing-body aerodynamic interaction on space shuttle subsonic flutter (National Aeronautics and Space Administration ;, 1975), also by Richard R. Chipman, Frank J. Rauch, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: An automated procedure for computing the three-dimensional transonic flow over wing-body combinations, including viscous effects. Volume II, Program unser's manual and code description. Appendix A, Computer code listing and flowchart (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1977., 1977), also by William H. Mason, Juanita Frick, W. F. Ballhaus, Mark Stern, Donald Mackenzie, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Grumman Aerospace Corporation: An automated procedure for the optimization of practical aerospace structures. Volume 1, Theoretical development and user's information (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971., 1971), also by Walter J. Dwyer, Irving U. Ojalvo, Robert K. Emerton, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Grumman Aerospace Corporation: An automated procedure for the optimization of practical aerospace structures. Volume 2, Programmer's manual (Air Force Flight Dynamicsl Laboratory, Air Force Systems Command, United States Air Force, 1971), also by Walter J. Dwyer, Patricia L. Sabatelli, Robert K. Emerton, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Grumman Aerospace Corporation: Control definition study for advanced vehicles (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Maris Lapins, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
• Grumman Aerospace Corporation: Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume I-computational technique (U.S. National Aeronautics and Space Administration ;, 1976), also by Frank Marconi, Larry Yaeger, Manuel Salas, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: Development of a computer code for calculating the steady super/hypersonic inviscid flow around real configurations : volume II - code description (U.S. National Aeronautics and Space Administration ;, 1976), also by Frank Marconi, Larry Yaeger, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Development of an apparatus to measure thermophysical properties of wind tunnel heat transfer models (National Aeronautics and Space Administration ;, 1974), also by Richard F. Romanowski, Ira H. Steinberg, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Development of immobilized enzyme systems for enhancement of biological waste treatment processes ([Environmental Protection Agency, Water Quality Office]; for sale by the Supt. of Docs., U.S. Govt. Print. Off., 1970), also by Lawrence Slote and United States. Environmental Protection Agency. Water Quality Office (page images at HathiTrust)
• Grumman Aerospace Corporation: Ditching investigation of a 1/20-scale model of the space shuttle orbiter (National Aeronautics and Space Administration ;, 1975), also by William L. Thomas and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: DYCAST, a finite element program for the crash analysis of structures (National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1987), also by A. Pifko, P. L. Ogilvie, R. Winter, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Electrochemical photovoltaic cells CdSe thin film electrodes : final report, June 1979-June 1980 (Golden, Colorado : Solar Energy Research Institute ; Springfield, Virginia : Available from National Technical Information Service, 1980., 1980), also by Michael A. Russak, Charles Creter, Jerome DeCarlo, Joseph Reichman, Mo.) Midwest Research Institute (Kansas City, and Solar Energy Research Institute (page images at HathiTrust)
• Grumman Aerospace Corporation: Experimental investigation of orthotropic panel flutter at arbitrary yaw angles, and comparison with theory (National Aeronautics and Space Administration ;, 1973), also by Peter Shyprykevich and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Field testing of prototype acoustic emission sewer flowmeter (Cincinnati, Ohio : Municipal Environmental Research Laboratory, Office of Research and Development, U.S. Environmental Protection Agency, 1979., 1979), also by K. M. Foreman and Municipal Environmental Research Laboratory (page images at HathiTrust)
• Grumman Aerospace Corporation: Finite element modeling and optimization of aerospace structures (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1972., 1972), also by Walter J. Dwyer, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
• Grumman Aerospace Corporation: Flutter analysis and testing of pairs of aerodynamically interfering delta wings (National Aeronautics and Space Administration ;, 1973), also by Richard R. Chipman, Frank J. Rauch, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: A guide for predicting the vibrations of fighter aircraft in the preliminary design stages (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Systems Command, United States Air Force, 1973., 1973), also by Eric E. Ungar, Air Force Flight Dynamics Laboratory (U.S.), and Beranek Bolt (page images at HathiTrust)
• Grumman Aerospace Corporation: Heat transfer distributions induced by elevon deflections on swept wings and adjacent surfaces at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1978), also by Charles B. Johnson, Louis G. Kàufman, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Grumman Aerospace Corporation: An improved supersonic, three-dimensional, external, inviscid flow field code (National Aeronautics and Space Administration, Scientific and Technical Information Office ;, 1979), also by Frank Marconi, Frank Koch, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)
• Grumman Aerospace Corporation: Investigation of hydrogen-air ignition senitized by nitric oxide and by nitrogen dioxide (National Aeronautics and Space Administration ;, 1977), also by M. Slack, A. Grillo, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: Lateral conduction effects on heat-transfer data obtained with the phase-change paint technique (National Aeronautics and Space Administration ;, 1974), also by George Maise, Michael J. Rossi, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: NASA TN D-5794 (National Aeronautics and Space Administration :, 1970), also by P. Caruso, Goddard Space Flight Center, and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: The NCOREL computer program for 3D nonlinear supersonic potential flow computations (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1983), also by Michael J. Siclari, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: 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 Lockheed-Georgia Company (page images at HathiTrust)
• Grumman Aerospace Corporation: 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 Lockheed-Georgia Company (page images at HathiTrust)
• Grumman Aerospace Corporation: 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 Lockheed-Georgia Company (page images at HathiTrust)
• Grumman Aerospace Corporation: 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 Lockheed-Georgia Company (page images at HathiTrust)
• Grumman Aerospace Corporation: Numerical nonlinear inelastic analysis of stiffened shells of revolution (National Aeronautics and Space Administration ;, 1975), also by V. Svalbonas, P. Ogilvie, and Harold Levine (page images at HathiTrust)
• Grumman Aerospace Corporation: A numerically efficient finite element hydroelastic analysis : volume 1--theory and results (U.S. National Aeronautics and Space Administration ;, 1976), also by Robert N. Coppolino and United States National Aeronautics and Space Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: A passive flow measurement system for storm and combined sewers (U.S. Environmental Protection Agency, Office of Research and Development, Municipal Environmental Research Laboratory ;, 1976), also by K. M. Foreman and United States. Environmental Protection Agency. Office of Research and Development (page images at HathiTrust)
• Grumman Aerospace Corporation: PLANS : a finite element program for nonlinear analysis of structures. Volume I, Theoretical manual (National Aeronautics and Space Administration, 1975), also by A. Pifko, Harry Armen, H. S. Levine, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Prevention of preferential bridge icing using heat pipes (Dept. of Transportation, Federal Highway Administration, Office of Research ;, 1977), also by Angelo A. Ferrara, George Yenetchi, and United States. Federal Highway Administration. Office of Research (page images at HathiTrust)
• Grumman Aerospace Corporation: Prevention of preferential bridge icing using heat pipes : interim report (Federal Highway Administration, Office of Research & Development ;, 1975), also by Angelo A Ferrara, R Haslett, and United States Federal Highway Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: Random vibration : decrease corporate cost increase fleet readiness (Dept. of the Navy, 1978), also by United States. Navy Dept. Electronic Systems Command (page images at HathiTrust)
• Grumman Aerospace Corporation: Simulation of a hydrocarbon fueled scramjet exhaust (National Aeronautical and Space Administration, Scientific and Technical Information Branch ;, 1982), also by J. Leng, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Simulation of hypersonic scramjet exhaust (National Aeronautics and Space Administration ;, 1975), also by R. A. Oman and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: A study of the implications of applying quantitative risk criteria in the licensing of nuclear power plants in the United States (Division of Systems and Reliability Research, Office of Nuclear Regulatory Research, U.S. Nuclear Regulatory Commission :, 1981), also by S. Mitra, A. Coppola, R. Hall, U.S. Nuclear Regulatory Commission. Division of Systems and Reliability Research, and Brookhaven National Laboratory (page images at HathiTrust)
• Grumman Aerospace Corporation: Thermal dynamic modeling study (National Aeronautics and Space Administration ;, 1972), also by I. U. Ojalvo and Langley Research Center (page images at HathiTrust)
• Grumman Aerospace Corporation: Tracked air cushion research vehicle subsystems analysis (The Dept. ;, 1971), also by A. Schlosser and United States. Office of High-Speed Ground Transportation (page images at HathiTrust)
• Grumman Aerospace Corporation: Tracked levitated research vehicle : periodic test summary report : primary suspension-aeropropelled (Federal Railroad Administration, Office of Research, Development and Demonstrations :, 1976), also by G. Fischer, B. Zapotowski, and United States. Federal Railroad Administration (page images at HathiTrust)
• Grumman Aerospace Corporation: Validation of scramjet exhaust simulation technique (National Aeronautics and Space Administration ;, 1976), also by H. B. Hopkins, J. Leng, H. B. Konopka, United States National Aeronautics and Space Administration, and Langley Research Center (page images at HathiTrust)

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