Books by Calvin Wayne Dahlke:
Books in the extended shelves:
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Dahlke, Calvin Wayne: Aerodynamic characteristics of wraparound fins mounted on bodies of revolution and rheir influence on the missile static stability at Mach numbers from 0.3 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by Joseph C. Craft, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)- Dahlke, Calvin Wayne: Aerodynamics of longitudinally supported ring tail configurations (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Aeroballistics Directorate, 1971., 1971), also by Redstone Arsenal (Ala.) and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: An experimental investigation of downstream flow-field properties behind a forward located sonic jet injected into transonic freestream from a body of revolution (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1968., 1968), also by Redstone Arsenal (Ala.) and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: An experimental investigation of downstream flow-field properties behind a sonic jet injected into transonic free stream from a body of revolution : Series II (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1969., 1969), also by Redstone Arsenal (Ala.) and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: An experimental investigation using a normal jet plume simulator to determine jet plume effects on a long slender rocket configuration at Mach numbers from 0.2 to 1.5 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James H Henderson, G. Batiuk, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: An investigation of flow and stability characteristics for a body of revolution with fins and flare in presence of Plume induced separation at Mach numbers 0.7 to 1.4 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, Aeroballistics Direcorate, Technology Laboratory, 1977., 1977), also by Redstone Arsenal (Ala.) and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 0.5 to 1.3 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, Advanced Systems Laboratory, Research and Engineering Directorate, 1972., 1972), also by John E. Vaughn, Joseph C. Craft, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: Static aerodynamic stability characteristics of a body of revolution with wraparound fins at Mach numbers from 1.6 to 2.86 (Redstone Arsenal, Alabama ; U.S. Army Missile Command, 1972., 1972), also by John E. Vaughn, Joseph C. Craft, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
- Dahlke, Calvin Wayne: A summary of aerodynamic characteristics for wrap-around fins from Mach 0.3 to 3.0 (Redstone Arsenal, Alabama ; U.S. Army Missile Research and Development Command, 1977., 1977), also by James A. Humphrey, Redstone Arsenal (Ala.), and United States. Army. Missile Command (page images at HathiTrust)
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