THE CORRECTION OF FLEXIBLE PLATE SUPERSONIC NOZZLE CONTOURS BY INFLUENCE METHODS

Open PDF

Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1953
Accession Number
AD0030950

Entities

People

  • W. N. Macdermott

Organizations

  • Arnold Engineering Development Complex

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Boundary Layer
  • Flow
  • Flow Fields
  • Jet Propulsion
  • Layers
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Shock Waves
  • Simultaneous Equations
  • Stagnation Pressure
  • Supersonic Nozzles
  • Supersonic Wind Tunnels
  • Turbulent Boundary Layer
  • Turbulent Mixing
  • Wind Tunnels

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Boundary Layers