The Reversibility Theorem for Thin Airfoils in Subsonic and Supersonic Flow.

Abstract

NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1950
Accession Number
ADA298731

Entities

People

  • Clinton E. Brown

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Materials and Manufacturing Processes

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Air Force
  • Airfoils
  • Boundary Layer
  • Engineering
  • Equations
  • Flow
  • Fluid Flow
  • Leading Edges
  • Momentum
  • Reynolds Number
  • Standards
  • Supersonic Flow
  • Surfaces
  • Trailing Edges
  • United States

Technology Areas

  • Hypersonics