Accession Number:

AD0754920

Title:

Static Stability and Axial Force Characteristics of Several Flat-Faced Right Circular Cylinders at Subsonic and Supersonic Speeds and Angles of Attack from 0 to 90 Degrees

Descriptive Note:

Final rept. 6-13 Jul 1972

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN

Personal Author(s):

Report Date:

1973-01-01

Pagination or Media Count:

87.0

Abstract:

Tests were conducted at Mach numbers from 0.2 to 0.8 and 1.5 to 2.5 to determine the effects of fineness ratio and angles of attack up to 90 degrees on the static longitudinal stability and axial force of a flat-faced cylinder. Tabulated and plotted data for the entire test matrix are presented.

Subject Categories:

  • Gliders and Parachutes
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE