Tables of Inviscid Supersonic Flow About Circular Cones at Incidence Gamma = 1.4. Part 2

Abstract

Statistical data are given for Mach 1.5 to Mach 20.0.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1969
Accession Number
AD0698780

Entities

People

  • D. J. Jones

Organizations

  • AGARD

Tags

Communities of Interest

  • C4I

DTIC Thesaurus Topics

  • Bodies
  • Coefficients
  • Computational Science
  • Dynamics
  • Flow
  • Fluid Dynamics
  • Fluid Mechanics
  • Image Motion Compensation
  • Mechanics
  • Physics
  • Slender Bodies
  • Statistical Data
  • Supersonic Flow

Fields of Study

  • Physics

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers
  • Hypersonics - Hypersonic Flow