Tables of Inviscid Supersonic Flow about Circular Cones at Incidence Gamma Equals 1.4. Part 3

Abstract

The report provides tabulated results for half cone angles of 45, 47.5, 50, 52.5, 55 and 57 degrees with Mach numbers ranging from 3 to 20.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1971
Accession Number
AD0736313

Entities

People

  • D. J. Jones

Organizations

  • AGARD

Tags

Communities of Interest

  • Space

DTIC Thesaurus Topics

  • Abstracts
  • Accuracy
  • Coefficients
  • Computational Science
  • Coordinate Systems
  • Differential Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fourier Series
  • Mach Number
  • National Security
  • Shock
  • Shock Waves
  • Space Stations
  • Specific Heat
  • Supersonic Flow

Fields of Study

  • Physics

Technology Areas

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