ON THE FLOW AT THE REAR OF A TWO-DIMENSIONAL SUPERSONIC AIRFOIL WITH THICKNESS

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Document Details

Document Type
Technical Report
Publication Date
May 01, 1953
Accession Number
AD0009822

Entities

People

  • Ronald F. Probstein

Organizations

  • Princeton University

Tags

DTIC Thesaurus Topics

  • Air Force
  • Airfoils
  • Deflection
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Mach Number
  • Military Research
  • New York
  • Power Series
  • Scientific Research
  • Shock
  • Shock Waves
  • Static Pressure
  • Supersonic Airfoils
  • Two Dimensional
  • Waves

Technology Areas

  • Hypersonics