TABLES OF SUPERSONIC FLOW AROUND YAWING CONES

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.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1947
Accession Number
AD0684051

Entities

Organizations

  • Massachusetts Institute of Technology

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Axial Flow
  • Differential Equations
  • Equations
  • Flight
  • Flow
  • Free Stream
  • Insensitive Explosives
  • Mach Number
  • Navy
  • Photographs
  • Photography
  • Physical Properties
  • Radial Velocity
  • Shock Waves
  • Supersonic Flight
  • Supersonic Flow
  • United States

Fields of Study

  • Physics

Readers

  • Calculus or Mathematical Analysis
  • Fluid Dynamics.
  • Forest Ecology

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers