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

Subject Categories:

Distribution Statement:

APPROVED FOR PUBLIC RELEASE