FLIGHT INVESTIGATION OF THE EFFECTS OF A PARTIAL-SPAN LEADING-EDGE CHORD EXTENSION ON THE AERODYNAMIC CHARACTERISTICS OF A 35 deg SWEPT-WING FIGHTER AIRPLANE

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Document Details

Document Type
Technical Report
Publication Date
Apr 23, 1954
Accession Number
AD0029198

Entities

People

  • Frederick H. Matteson
  • Rudolph D. Van Dyke Jr.

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aircrafts
  • Airframes
  • Airplanes
  • Computational Fluid Dynamics
  • Fighter Aircraft
  • Flow
  • High Lift
  • Leading Edges
  • Mach Number
  • Measurement
  • Swept Wings
  • Sweptback Wings
  • Tangents
  • Trailing Edges
  • Vortex Generators