ADVANCED AERODYNAMIC SPIKE CONFIGURATIONS

Abstract

Investigations of the aerodynamic spike nozzle concept are discussed in this report. Cold-flow test programs to evaluate high area ratio aerodynamic spike nozzles and combustion configurations for aerodynamic spike nozzles were completed. A description of the models tested and the test results are presented. Analytical and design studies of the aerodynamic spike nozzle concept were conducted and the results are presented.

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1966
Accession Number
AD0378296

Entities

People

  • Roy Silver

Tags

Communities of Interest

  • Weapons Technologies

DTIC Thesaurus Topics

  • Air Force
  • Altitude
  • Base Flow
  • Base Pressure
  • Bell Nozzles
  • Boundary Layer
  • Combustion
  • Combustion Chambers
  • Flow Fields
  • Heat Transfer
  • High Pressure
  • Jet Propulsion
  • Lepidoptera
  • Propulsion Systems
  • Rocket Propulsion
  • Thrust Chambers
  • Wake

Fields of Study

  • Physics

Readers

  • Combustion and Flow Dynamics.
  • Electrical Engineering