A Study of Flow Changes Associated with Airfoil Section Drag Rise at Supercritical Speeds

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Document Details

Document Type
Technical Report
Publication Date
Feb 01, 1949
Accession Number
ADA380638

Entities

People

  • Gerald E. Nitzberg
  • Stewart Crandall

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Airfoils
  • Boundaries
  • Boundary Layer
  • Coefficients
  • Dynamic Pressure
  • Flow
  • Free Stream
  • Low Drag
  • Low Drag Airfoils
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Shock Waves
  • Static Pressure
  • Supercritical Flow
  • Supersonic Flow