Flight Tests to Determine the Effect of Airfoil Section Profile and Thickness Ratio on the Zero-Lift Drag of Low-Aspect Ratio Wings at Supersonic Speeds

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Document Details

Document Type
Technical Report
Publication Date
Feb 09, 1948
Accession Number
ADA800791

Entities

People

  • Ellis Katz

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Aircrafts
  • Airfoils
  • Aspect Ratio
  • Boundary Layer
  • Coefficients
  • Drag
  • Flow
  • Flow Fields
  • Free Stream
  • Leading Edges
  • Mach Number
  • Supersonic Flow
  • Swept Wings
  • Sweptback Wings

Technology Areas

  • Hypersonics
  • Hypersonics - Hypersonic Flow