Books by Louis G. Kaufman:
Books in the extended shelves:
![[X-Info]](https://onlinebooks.library.upenn.edu/infouc.gif)
Kàufman, Louis G.: 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, Grumman Aerospace Corporation, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office (page images at HathiTrust)- Kaufman, Louis G.: High speed flow separation ahead of finite span steps (Wright-Patterson Air Force Base, Ohio : Air Force Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, 1978., 1978), also by Robert D. Kirchner, Air Force Flight Dynamics Laboratory (U.S.), and United States. Air Force. Systems Command (page images at HathiTrust)
- Kaufman, Louis G.: Interference heating from interactions of shock waves with turbulent boundary layers at Mach 6 (National Aeronautics and Space Administration ;, 1974), also by Charles B. Johnson and Langley Research Center (page images at HathiTrust)
- Kaufman, Louis G.: 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 Daniel Weiss, Stravos Hartofilis, Lawrence Meckler, United States. Air Force. Systems Command. Research and Technology Division, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
- Kaufman, Louis G.: Mach 0.6 to 3.0 flows over rectangular cavities (Wright-Patterson Air Force Base, Ohio : Flight Dynamics Laboratory, Air Force Wright Aeronautical Laboratories, Air Force Systems Command, United States Air Force, 1983., 1983), also by Rodney L. Clark, Algirdas Maciulaitis, Air Force Wright Aeronautical Laboratories, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aerospace Corporation. Research and Development Center (page images at HathiTrust)
- Kàufman, Louis G.: Methods for estimating pressure and thermal loads induced by elevon deflections on hypersonic-vehicle surfaces with turbulent boundary layers (National Aeronautics and Space Administration, Scientific and Technical Information Branch ;, 1981), also by Charles B. Johnson, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch (page images at HathiTrust)
- Kaufman, Louis G.: 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 Lawrence Meckler, Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, Grumman Aircraft Engineering Corporation. Research Department, and Wright-Patterson Air Force Base (Ohio) (page images at HathiTrust)
- Kaufman, Louis G.: 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 Air Force Flight Dynamics Laboratory (U.S.), United States. Air Force. Systems Command. Aeronautical Systems Division, and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
- Kaufman, Louis G.: 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 United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), Grumman Aircraft Engineering Corporation. Research Department, and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
- Kaufman, Louis G.: 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 United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
- Kaufman, Louis G.: Pressure and thermal distributions on wings and adjacent surfaces induced by elevon deflections at Mach 6 (National Aeronautics and Space Administration, Scientific and Technical Information Office, 1979), also by Charles B. Johnson (page images at HathiTrust)
- Kaufman, Louis G.: 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 United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation. Research Department (page images at HathiTrust)
- Kaufman, Louis G.: 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 United States. Air Force. Systems Command, Air Force Flight Dynamics Laboratory (U.S.), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
- Kaufman, Louis G.: Real gas flow tables for nondissociated air (Wright-Patterson Air Force Base, Ohio : Wright Air Development Center, Air Research and Development Command, United States Air Force, 1959., 1959), also by Wright Air Development Center, United States. Air Force. Air Research and Development Command, and Aero Medical Laboratory (United States. Army Air Forces) (page images at HathiTrust)
- Kaufman, Louis G.: 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 Daniel Weiss, Lawrence H. Meckler, Richard A. Oman, William J. Evans, Stravros A. Hartofilis, United States. Air Force. Systems Command. Aeronautical Systems Division, Wright-Patterson Air Force Base (Ohio), and Grumman Aircraft Engineering Corporation (page images at HathiTrust)
- Kaufman, Louis G.: Weak incident shock interactions with Mach 8 laminar boundary layers (National Aeronautics and Space Administration ;, 1974), also by Charles B. Johnson and Langley Research Center (page images at HathiTrust)
Find more by Louis G. Kaufman at your library, or elsewhere.