Accession Number:
AD0256174
Title:
PRESSURE DISTRIBUTION ON A BLUNTED 15 DEGREES CIRCULAR CONE
Descriptive Note:
Technical rept.
Corporate Author:
GENERAL APPLIED SCIENCE LABS INC HEMPSTEAD N Y
Personal Author(s):
Report Date:
1960-02-01
Pagination or Media Count:
1.0
Abstract:
Results are presented for an experimental wind tunnel investigation conducted at Mach 8. The effect of angle of attack and of Reynolds number variation on the pressure distribution on a blunted 15 degree semi-vortex angle right circular cone of 0.40-in. nose radius and 10.75-in. length is considered. Axial and peripheral pressure distributions are presented. Several existing theories are included and comparisons are made between them and experimental results. Author