Online Books by
Grumman Aircraft Engineering Corporation
Books from the extended shelves:
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Grumman Aircraft Engineering Corporation: The calculation of nonlinear supersonic conical flows by the method of integral relations (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by John W. Brook, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Aeronautical Research Associates of Princeton (page images at HathiTrust)- Grumman Aircraft Engineering Corporation: A conical thin-shock-layer theory uniformly valid in the entropy layer (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 Robert E. Melnik, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), Wright-Patterson Air Force Base. Flight Dynamics Laboratory, and Aeronautical Research Associates of Princeton (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Experimental measurements of forces at Mach 8 and pressures at Mach 21 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Harold R. Mead, Stavros A. Hartofilis, Frank Koch, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Experimental pressure measurements at Mach 5 and 8 (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Harold R. Mead, Frank Koch, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, United States. Aerospace Medical Division, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Final test report : X-29A Vortex Flow Control (VFC) flight test results (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Directorate , Wright Laboratory, Air Force Materiel Command, United States Air Force, 1993., 1993), also by Frank Luria, Brian Hobbs, Paul Pellicano, Joseph Krumenacker, William Gillard, and Ohio) Wright Laboratory (Wright-Patterson Air Force Base (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Hypersonic flow theories for predicting pressures on blunt two-dimensional and on conical shapes (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1964), also by Richard A. Scheuing, Roger D. Sullivan, Coleman duP. Donaldson, Wallace D. Hayes, John W. Brook, Robert E. Melnik, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Aeronautical Research Associates of Princeton (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Investigation of dynamic stability derivatives of vehicles flying at hypersonic velocity (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Arthur Gilmore, Donald Mackenzie, Vladimir Seredinsky, and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: An investigation of hypersonic flow separation and 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, 1965., 1965), also by Louis G. Kaufman, Daniel Weiss, Stravos Hartofilis, Lawrence Meckler, United States. Air Force. Systems Command. Research and Technology Division, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Investigation of pressure distributions over planar, twisted, and cambered wings in a hypersonic wind tunnel (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by H. B. Hopkins, J. Leng, Richard A. Scheuing, United States. Air Force. Systems Command. Aeronautical Systems Division, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Matrix analysis methods for anisotropic inelastic structures (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 W. R. Jensen, N. Prince, W. E. Falby, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Operational testing and evaluation of the hydrofoil seacraft Denison : from June 1962 through 1963 (Grumman, 1963), also by United States Maritime Administration (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Pressure and heat transfer measurements for Mach 21 flows over a blunt pyramidal configuration with aerodynamic controls : part of an investigation of hypersonic flow separation and 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, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Pressure measurement at Mach 19 for a winged re-entry configuration : part of an investigation of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Flight Control Division, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Stavros A. Hartofilis and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part II. Conical cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Pressure measurements for mach five flows over winged re-entry configurations with aerodynamic controls. Part 1. Blunt cabin configuration (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, United States Air Force, 1964., 1964), also by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), and Wright-Patterson Air Force Base. Flight Dynamics Laboratory. Research and Technology Division (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: A review of hypersonic flow separation and control characteristics (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Louis G. Kaufman, Daniel Weiss, Lawrence H. Meckler, Richard A. Oman, William J. Evans, Stravros A. Hartofilis, United States. Air Force. Systems Command. Aeronautical Systems Division, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
- Grumman Aircraft Engineering Corporation: Theoretical prediction of pressures in hypersonic flow with special reference to configurations having attached leading-edge shock. Part 1. Theoretical investigation (Wright-Patterson Air Force Base, Ohio : Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1962., 1962), also by Richard A. Scheuing, Robert E. Melnik, John W. Brook, Harold R. Mead, Aeronautical Research Associates of Princeton, United States. Air Force. Systems Command. Aeronautical Systems Division, United States. Air Force. Systems Command. Aeronautical Systems Division. Directorate of Materials and Processesd States, and United States. Aerospace Medical Division (page images at HathiTrust)
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