Flight-Test Evaluation of the Longitudinal Stability and Control Characteristics of 0.5-Scale Models of the Fairchild Lark Pilotless-Aircraft Configuration. Standard Configuration with Wing Flaps Deflected 60 deg and Model Having Tail in Line with Wings. TED No. NACA 2387

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Document Details

Document Type
Technical Report
Publication Date
Jun 25, 1947
Accession Number
ADA801235

Entities

People

  • David G. Stone

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Aeronautics
  • Aircrafts
  • Blast Tubes
  • Center Of Gravity
  • Control Surfaces
  • Flaps (Control Surfaces)
  • Free Stream
  • Mach Number
  • Navy
  • Photographs
  • Rocket Engines
  • Scale Models
  • Surfaces
  • Test And Evaluation
  • Unmanned Aerial Vehicles
  • Wing Flaps