Investigation at Supersonic Speeds of the Effect of Jet Mach Number and Divergence Angle of the Nozzle upon the Pressure of the Base Annulus of a Body of Revolution

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 17, 1954
Accession Number
AD0048258

Entities

People

  • August F. Bromm Jr.
  • Robert M. O'donnell

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Base Pressure
  • Bodies
  • Boundary Layer
  • Conical Nozzles
  • Diameters
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Jet Flow
  • Mach Number
  • Measurement
  • Nozzles
  • Pressure Measurement
  • Stagnation Pressure
  • Static Pressure
  • Supersonic Nozzles

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow