Accession Number:

AD0684051

Title:

TABLES OF SUPERSONIC FLOW AROUND YAWING CONES

Descriptive Note:

Technical rept.

Corporate Author:

MASSACHUSETTS INST OF TECH CAMBRIDGE CENTER OF ANALYSIS

Personal Author(s):

Report Date:

1947-01-01

Pagination or Media Count:

336.0

Abstract:

Contents Tables of supersonic flow of air around slightly yawing cones of the following semi-apex angles Survey of the results Table giving the shock-to-cone ratio in terms of the radial velocity-component along the solid surface and the semi-apex angle of the cone Table giving the coefficient of normal drag in terms of the radial velocity-component along the solid surface and the semi-apex angle of the cone Diagrams illustrating some physical properties of supersonic flow of air around slightly yawing cones.

Subject Categories:

  • Aerodynamics
  • Fluid Mechanics

Distribution Statement:

APPROVED FOR PUBLIC RELEASE