The Online Books Page

Books by Grumman Aircraft Engineering Corporation. Research Department:

Books in the extended shelves:

• Grumman Aircraft Engineering Corporation. Research Department: Aerodynamic characteristics and flap loads for a blunt pyramidal configuration at Mach 5 and 8 : 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 William J. Evans, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Experimental investigation of pressures on a blunt two-dimensional profile and on sharp and blunt conical shapes of noncircular cross section at Mach 5 and 8 (Wright-Patterson Air Force Base, Ohio : Flight Control Laboratory, Aeronautical Systems Division, Air Force Systems Command, United States Air Force, 1963., 1963), also by Harold R. Mead, Frank Koch, United States. Air Force. Systems Command. Aeronautical Systems Division, Air Force Flight Dynamics Laboratory (U.S.), and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Heat transfer measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : 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 Lawrence Meckler, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure and heat transfer measurements at mach 13 and 19 for flows ahead of ramps, over expansion corners, and past fin-plate combinations : 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 Stavros A. Hartofilis, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure and heat transfer measurements at Mach 5 and 8 for a fin-flat plate model : part of an investigation 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, 1963., 1963), also by Louis G. Kaufman, Lawrence Meckler, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure and heat transfer measurements for hypersonic flows over expansion corners and ahead of ramps (Air Force Flight Dynamics Laboratory, Research and Technology Division, Air Force Systems Command, 1963), also by Louis G. Kaufman, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command. Aeronautical Systems Division (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: 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 (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure and heat transfer measurements for Mach 8 flows over a blunt pryamidal configuration with aerodynamic controls. Part I. Pressure data for delta wing surface (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. Research Department: Pressure and heat transfer measurements for Mach 8 flows over a blunt pyramidal configuration with aerodynamic controls (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. Research Department: Pressure measurements at Mach 8 on an aerodynamically controllable winged re-entry configuration : 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, 1965., 1965), also by Lawrence Meckler, United States. Air Force. Systems Command, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 2. Flows over a flat plate with and without a partial span ramp : 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, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Pressure measurements for Mach 8 flows over expansion corners and ramps on an internally cooled model. Part 3 Flows over full span ramps mounted on a flat plate (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. Research Department: Pressure measurements for Mach five 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, and Air Force Flight Dynamics Laboratory (U.S.) (page images at HathiTrust)
• Grumman Aircraft Engineering Corporation. Research Department: Static aerodynamic characteristics at Mach 5 and 8 of an aerodynamically controllable winged re-entry configuration : 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, 1963., 1963), also by Lawrence Meckler, United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Wright-Patterson Air Force Base. Flight Dynamics Laboratory (page images at HathiTrust)

Find more by Grumman Aircraft Engineering Corporation. Research Department at your library, or elsewhere.