Pressure-Distribution Measurements on a Full-Scale Horizontal Tail Surface for a Mach Number Range of 0.20 to 0.70

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Document Details

Document Type
Technical Report
Publication Date
Jun 25, 1947
Accession Number
ADA801031

Entities

People

  • Carl F. Schueller

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Airplanes
  • Buildings And Structures
  • Coefficients
  • Free Stream
  • Horizontal Stabilizers
  • Mach Number
  • Measurement
  • Physical Properties
  • Pressure Distribution
  • Stabilization Systems
  • Surfaces
  • Test Facilities
  • Wind Tunnels