High Mach Number Predictive Methods for Missile Configurations.

Abstract

This report provides an overview of the numerical research conducted on steady supersonic inviscid flows with crossflow separation during the period of May 1982 through May 1985. The publications resulting from that research are summarized.

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Document Details

Document Type
Technical Report
Publication Date
Jul 01, 1985
Accession Number
ADA158358

Entities

People

  • G. H. Klopfer

Organizations

  • Nielsen Engineering & Research (United States)

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Algorithms
  • Bow Shock
  • Computational Fluid Dynamics
  • Conformal Mapping
  • Contracts
  • Demographic Cohorts
  • Engineering
  • Equations
  • Errors
  • Euler Equations
  • Flow
  • Flow Fields
  • Fluid Flow
  • Inviscid Flow
  • Mach Number
  • Military Research
  • Supersonic Flow

Fields of Study

  • Physics

Readers

  • Aerodynamics.
  • Business Analytics

Technology Areas

  • Hypersonics