Stability Derivatives at Supersonic Speeds of Thin Rectangular Wings with Diagonals Ahead of Tip Mach Lines,

Abstract

NO ABSTRACT DUE TO ILLEGIBILITY OF REPORT (KAR)

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1949
Accession Number
ADA298303

Entities

People

  • Sidney M. Harmon

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aircraft Industry
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Boundary Layer
  • Equations
  • Flow
  • Free Stream
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Pressure Gradients
  • Skin Friction
  • Speed
  • Trailing Edges
  • Wing Tips

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow