Aerodynamic characteristics of 2-, 3-, and 4-, caliber tangent-ogive cylinders with nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 at Mach numbers from 0.6 to 4.0, by Carroll B. Butler et al.

Title:	Aerodynamic characteristics of 2-, 3-, and 4-, caliber tangent-ogive cylinders with nose bluffness ratios of 0.00, 0.25, 0.50, and 0.75 at Mach numbers from 0.6 to 4.0
Author:	Butler, Carroll B.
Author:	Pallas, Spiros Georgios, 1942-
Author:	Sears, Edward S. (Edward Seldon), 1943-
Author:	United States. Air Force. Systems Command
Author:	Air Force Armament Laboratory
Note:	Eglin Air Force Base, Florida : Air Force Armament Laboratory, Systems Analysis and Stimulation Branch, Guided Weapons Division, Air Force Systems Command, United States Air Force, 1977., 1977

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Subject:	Radomes
Subject:	Wind tunnel testing
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