The High-Speed Aerodynamic Effects of Modifications to the Wing and Wing-Fuselage Intersection of an Airplane Model with the Wing Swept Back 35 deg

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Document Details

Document Type
Technical Report
Publication Date
Feb 18, 1948
Accession Number
ADA800786

Entities

People

  • Charles P. Morrill Jr.
  • Lee E. Boddy

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Flow
  • Aircrafts
  • Airfoils
  • Airplanes
  • Boundary Layer
  • Free Stream
  • Leading Edges
  • Mach Number
  • Pressure Distribution
  • Pressure Measurement
  • Static Pressure
  • Surfaces
  • Sweptback Wings
  • Trailing Edges
  • Wind Tunnel Tests
  • Wind Tunnels