General Slender Cone Simulation at Reentry Flow Conditions

Abstract

By using the results of general similarity, the problem of modeling the hypersonic flow about a reentry cone is reviewed. The techniques developed are applied to a specific proposed ballistic range experiment.

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1977
Accession Number
ADA041063

Entities

People

  • Joseph A. Johnson Iii

Organizations

  • Rutgers University–New Brunswick

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Air Force
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Electron Density
  • Engineering
  • Equations
  • Flow
  • Flow Fields
  • Fluid Dynamics
  • Fluid Flow
  • Froude Number
  • Gas Flow
  • Heat Transfer
  • Mach Number
  • Simulations
  • United States

Readers

  • Computational Modeling and Simulation
  • Fluid Dynamics.
  • Missile Defense Systems.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers