THE DESIGN OF VARIABLE MACH NUMBER ASYMMETRIC SUPERSONIC NOZZLES BY TWO PROCEDURES EMPLOYING INCLINED AND CURVED SONIC LINES

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Mar 01, 1953
Accession Number
AD0005154

Entities

People

  • Clarence A. Syvertson
  • Raymond C. Savin

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Boundaries
  • Boundary Layer
  • Coordinate Systems
  • Curvature
  • Dynamic Pressure
  • Flow
  • Flow Fields
  • Geometry
  • Leading Edges
  • Mach Number
  • Pressure Gradients
  • Static Pressure
  • Supersonic Flow
  • Supersonic Nozzles
  • Two Dimensional
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow