Stability of Compressible Wake and Jet Flows.

Abstract

In this report the stability of compressible inviscid jets and wakes has been investigated for various wave numbers and Mach numbers for different velocity profiles. (Author)

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1983
Accession Number
ADA136541

Entities

People

  • G. R. Verma
  • S. J. Scherr
  • W. L. Hankey

Organizations

  • Wright Laboratory

Tags

DTIC Thesaurus Topics

  • Aerodynamics
  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Boundary Layer
  • Dynamics
  • Eigenvalues
  • Equations
  • Flow
  • Government Procurement
  • Governments
  • Jet Flow
  • Layers
  • Mach Number
  • Mechanics
  • Security
  • Two Dimensional

Fields of Study

  • Physics