THE EFFECTS OF NACELLES AND OF EXTENDED SPLIT FLAPS ON THE LONGITUDINAL CHARACTERISTICS OF A WING-FUSELAGE-TAIL COMBINATION HAVING A WING WITH 40 DEGREES OF SWEEPBACK AND AN ASPECT RATIO OF 10

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Document Details

Document Type
Technical Report
Publication Date
Jun 01, 1953
Accession Number
AD0011175

Entities

People

  • Armando E. Lopez
  • Bruce E. Tinling

Organizations

  • National Aeronautics and Space Administration

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamic Forces
  • Aeronautical Laboratories
  • Aircrafts
  • Aspect Ratio
  • Coefficients
  • Deflection
  • Dynamic Pressure
  • Free Stream
  • Horizontal Stabilizers
  • Leading Edges
  • Mach Number
  • Reynolds Number
  • Split Flaps
  • Trailing Edges
  • Wind Tunnel Tests
  • Wind Tunnels