Accession Number : AD0223281
Title : PRESSURE DISTRIBUTION TESTS ON BLUNTED PLATE AND CONE AT MACH NUMBERS 20 TO 23,
Corporate Author : ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFS TN
Personal Author(s) : Wallace, A. R. ; Swain, W. N.
Report Date : JAN 1961
Pagination or Media Count : 31
Abstract : Pressure distribution tests were made on a blunted cone and a flat plate with two different nose radii in tunnel Hotshot 2 at Mach numbers 20 to 23 and Reynolds numbers about 300,000 per ft. Angle of attack ranged from 0 to 45 deg for the cone and from 0 to 30 deg for the flat plate. (Author)
Descriptors : (*BLUNT BODIES), (*AERODYNAMIC CONFIGURATIONS), (*CONICAL BODIES), (*HYPERSONIC CHARACTERISTICS), PRESSURE, DISTRIBUTION.
Distribution Statement : APPROVED FOR PUBLIC RELEASE