Stability Derivatives of Triangular Wings at Supersonic Speeds,

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1948
Accession Number
ADA298764

Entities

People

  • Frank S. Malvesstuto Jr
  • Herbert S. Ribner

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircraft Industry
  • Aircrafts
  • Aspect Ratio
  • Delta Wings
  • Engineering
  • Flight
  • Flow
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Reynolds Number
  • Skin Friction
  • Steady State
  • Two Dimensional
  • United States

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow