FLOW-FIELD EFFECTS ON STATIC STABILITY AND CONTROL AT HIGH SUPERSONIC MACH NUMBERS

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Document Details

Document Type
Technical Report
Publication Date
Mar 08, 1956
Accession Number
AD0093418

Entities

People

  • Edward F. Ulmann
  • Herbert W. Ridyard

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Airplanes
  • Control Surfaces
  • Dynamic Pressure
  • Flow
  • Flow Fields
  • Government Procurement
  • Governments
  • Horizontal Stabilizers
  • Leading Edges
  • Mach Number
  • Surfaces
  • United States
  • United States Government

Technology Areas

  • Hypersonics