Books by Lyle D. Kayser:
Books in the extended shelves:
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Kayser, Lyle D.: Boundary-layer trip effectiveness and computations of aerodynamic heating for XM797 nose-tip configurations (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1983., 1983), also by Walter B. Sturek, Donald C. Mylin, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)- Kayser, Lyle D.: Computational modeling of aerodynamic heating for XM797 nose cap configurations (Aberdeen Proving Ground, Maryland : U.S. Army Armament Research and Development Command, Ballistic Research Laboratory, 1983., 1983), also by Walter B. Sturek, Henry Hudgins, Donald C. Mylin, U.S. Army Ballistic Research Laboratory, and United States. Army Armament Research and Development Command (page images at HathiTrust)
- Kayser, Lyle D.: Computational study of swept-fin aerodynamic heating for the 105mm M774 (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1983., 1983), also by Walter B. Sturek, Paul Weinacht, and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
- Kayser, Lyle D.: Effects of base bleed and supersonic nozzle injection on base pressure (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratories, 1975., 1975), also by U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
- Kayser, Lyle D.: Some aerodynamic characteristics of a projectile shape with a nonaxisymmetric boattail at Mach numbers of 0.91 and 3.02 (Aberdeen Proving Ground, Maryland : U.S. Army Armament Research and Development Command, Ballistic Research Laboratory, 1983., 1983), also by Fred Whiton, U.S. Army Ballistic Research Laboratory, and United States. Army Armament Research and Development Command (page images at HathiTrust)
- Kayser, Lyle D.: Surface pressure measurements on a boattailed projectile shape at transonic speeds (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1982., 1982), also by F. Whiton and U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
- Kayser, Lyle D.: Wind tunnel tests on a nonaxisymmetric projectile shape at Mach numbers 2.5 to 6.0 (Aberdeen Proving Ground, Maryland : Ballistic Research Laboratory, 1983., 1983), also by U.S. Army Ballistic Research Laboratory (page images at HathiTrust)
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