STUDY OF FLOW OVER OSCILLATING AIRFOIL MODELS AT A MACH NUMBER OF 7.0 IN HELIUM

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1961
Accession Number
AD0268138

Entities

People

  • Ali Arman

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Boundary Layer
  • Computational Fluid Dynamics
  • Dynamic Pressure
  • Flow
  • Frequency
  • Leading Edges
  • Light Sources
  • Mach Number
  • Motion Pictures
  • Photographs
  • Shape
  • Shock Waves
  • Steady Flow
  • Steady State
  • Unsteady Flow
  • Waves
  • Wind Tunnels