An Empirically Derived Method for Calculating Pressure Distributions over Airfoils at Supercritical Mach Numbers and Moderate Angles of Attack

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Document Details

Document Type
Technical Report
Publication Date
Apr 01, 1947
Accession Number
ADA800830

Entities

People

  • Gerald E. Nitzberg
  • Loma E. Sluder

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Boundaries
  • Boundary Layer
  • Coefficients
  • Drag
  • Flow
  • Flow Fields
  • Layers
  • Low Drag
  • Mach Number
  • Motion
  • Pressure Distribution
  • Trailing Edges
  • Unsteady Flow