AN ANALYSIS OF THE FLUID MECHANICS OF SECONDARY INJECTION FOR THRUST VECTOR CONTROL (REVISED)

Abstract

An analysis is made of the interaction of an injected gas or liquid with a supersonic stream AND THE FORCE INDUCED ON AN ADJACENT WALL PREDICTED. The study deals only with the free stream-injectant interaction; the modifications to the flow intro uced by the boundary layer are not considered. In the case of liquids, it is shown that the momentum deficit of the injectant relative to the free stream may play a larger part in producing the side force than the volume generation by vaporization and reaction. The analytical results are compared with those obtained from experiments in a wind tunnel and in nozzles. (Author)

Document Details

Document Type
Technical Report
Publication Date
Mar 15, 1962
Accession Number
AD0283326

Entities

People

  • James E. Broadwell

Organizations

  • TRW Inc.

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Fluid Dynamics
  • Fluid Mechanics
  • Fluid Statics
  • Free Stream
  • Mechanics
  • Secondary Injection
  • Wind Tunnels

Fields of Study

  • Physics

Readers

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Technology Areas

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