Formulas for Source, Doublet, and Vortex Distributions in Supersonic Wing Theory

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1950
Accession Number
ADA382269

Entities

People

  • Franklyn B. Fuller
  • Harvard Lomax
  • Max A. Heaslet

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Boundary Value Problems
  • Complex Variables
  • Coordinate Systems
  • Differential Equations
  • Dynamic Pressure
  • Equations
  • Flow
  • Free Stream
  • Integral Equations
  • Mach Number
  • Mathematical Analysis
  • Partial Differential Equations
  • Theorems
  • Thickness
  • Trailing Edges
  • Wave Equations

Technology Areas

  • Hypersonics