Experimental Investigation of Reaction Jets on a Body of Revolution With and Without Fins in Supersonic Flow

Abstract

An experimental investigation of a sonic, underexpanded, transverse jet ejecting from a body of revolution into free streams of Mach number range 1. 75 to 4.5 was conducted. The jet was rolled, in 15-degree increments, into the yaw plane for an angle of attack range of -4 to + 10 degrees with a jet total-to-free stream static pressure ratio variations up to 100. Forces and moments were measured and the tabulated data are presented.

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Document Details

Document Type
Technical Report
Publication Date
May 30, 1970
Accession Number
AD0873490

Entities

People

  • Troy A. Street

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Base Pressure
  • Bodies
  • Coefficients
  • Dynamic Pressure
  • Export Controls
  • Flow
  • Free Stream
  • Government (Foreign)
  • Mach Number
  • Plastic Explosives
  • Revolutions
  • Reynolds Number
  • Static Pressure
  • Supersonic Flow
  • Transverse
  • Wind Tunnel Tests
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Fluid Mechanics and Fluid Dynamics.
  • ballistics.

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow