A Comparison at High Speed of the Aerodynamic Merits of Models of Medium Bombers Having Thickened Wing Roots and Having Wings with Nacelles

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1943
Accession Number
ADA801040

Entities

People

  • Eugene C. Draley

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Air Flow
  • Dynamic Pressure
  • Engine Nacelles
  • Free Stream
  • Fuselages
  • Leading Edges
  • Mach Number
  • Motion
  • Nacelles
  • Physical Properties
  • Pressure Distribution
  • Propeller Shafts
  • Propellers
  • Thickness
  • Two Dimensional