Accession Number:

AD0726533

Title:

Effect of Unsymmetrical Nose-Bluntness of the Pressure Distribution over a 10 Degree Cone at Mach-14.

Descriptive Note:

Final rept.,

Corporate Author:

AEROSPACE RESEARCH LABS WRIGHT-PATTERSON AFB OHIO

Report Date:

1971-03-01

Pagination or Media Count:

46.0

Abstract:

The pressure distribution over a 10 deg cone was measured in ARLs 20-inch hypersonic wind tunnel at Mach-14 and for various angles of attack and sideslip. The effect of different unsymmetrically blunted noses, with small bluntness ratios, on the pressure distribution is investigated. Test results relate any small unsymmetrical nose bluntness to the rotational symmetry of the flow over a body of revolution at high Mach numbers. The reported test complement, AD-711 921. Author

Subject Categories:

  • Guided Missile Dynamics, Configurations and Control Surfaces
  • Guided Missiles

Distribution Statement:

APPROVED FOR PUBLIC RELEASE