Accession Number:

AD0736313

Title:

Tables of Inviscid Supersonic Flow about Circular Cones at Incidence Gamma Equals 1.4. Part III.

Descriptive Note:

AGARDograph rept.,

Corporate Author:

ADVISORY GROUP FOR AEROSPACE RESEARCH AND DEVELOPMENT PARIS (FRANCE)

Personal Author(s):

Report Date:

1971-12-01

Pagination or Media Count:

173.0

Abstract:

The report provides tabulated results for half cone angles of 45, 47.5, 50, 52.5, 55 and 57 degrees with Mach numbers ranging from 3 to 20.

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE