Theoretical Investigation of Methods for Computing Drag from Wake Surveys at High Subsonic Speeds

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1945
Accession Number
ADB805967

Entities

People

  • Max A. Heaslet

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Agreements
  • Coefficients
  • Compressible Flow
  • Computations
  • Dynamic Pressure
  • Equations
  • Errors
  • Flow
  • Free Stream
  • Incompressible Flow
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Shape
  • Static Pressure