Accession Number:

AD0829024

Title:

LOW-SPEED WIND TUNNEL TESTS ON 15, 25, 40 AND 55 DEGREE SEMI-VERTEX ANGLE CONES TO DETERMINE THE SUPPORT EFFECTS ON FORCE COEFFICIENTS.

Descriptive Note:

Corporate Author:

GENERAL DYNAMICS SAN DIEGO CA CONVAIR DIV

Personal Author(s):

Report Date:

1958-03-10

Pagination or Media Count:

55.0

Abstract:

The primary purpose of this test was to determine the aerodynamic tare effects of the support on the cone force data and cone base pressure data. The cones were tested at dynamic pressures of 7.7, 26.2, 57.6, 104.7, 114.5, and 135.5 lbssq. ft. which correspond to Reynolds numbers of .475, .877, 1.300, 1.753, 1.833, and 1.994 million, respectively, based on a one-foot unit of length, an average test temperature of 91.4F and an average barometric pressure of 30.03 inches of mercury. Author

Subject Categories:

  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE