Flight Investigation at High Mach Numbers of Several Methods of Measuring Static Pressure on an Airplane Wing

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Document Details

Document Type
Technical Report
Publication Date
Nov 01, 1944
Accession Number
ADA801067

Entities

People

  • Fred L. Daum
  • John A. Zalovcik

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aircrafts
  • Airplanes
  • Airspeed
  • Boundaries
  • Boundary Layer
  • Flow
  • Fluid Dynamics
  • Leading Edges
  • Mach Number
  • Measurement
  • Pressure Distribution
  • Pressure Gradients
  • Pressure Measurement
  • Static Pressure
  • Subsonic Flow
  • Supersonic Flow