Accession Number:

AD0627317

Title:

A COMPARISON OF EXPERIMENTAL AND THEORETICALLY PREDICTED PRESSURE DISTRIBUTIONS AND FORCE AND STABILITY COEFFICIENTS FOR A SPHERICALLY BLUNTED CONE AT MACH APPROX. 18 AND ANGLES OF ATTACK

Descriptive Note:

Corporate Author:

ARNOLD ENGINEERING DEVELOPMENT CENTER ARNOLD AFB TN

Personal Author(s):

Report Date:

1966-02-01

Pagination or Media Count:

62.0

Abstract:

Analysis of experimental pressure distributions and force and moment coefficients for a 9-deg half-angle spherically blunted cone is presented based on an ideal gas y 1.4 three-dimensional characteristics solution developed by General Applied Sciences Laboratory GASL. Comparisons are also made with predictions based on modified Newtonian theory.

Subject Categories:

  • Military Aircraft Operations
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE