Free-Flight-Tunnel Investigation of the Effect of Mode of Propeller Rotation upon the Lateral-Stability Characteristics of a Twin-Engine Airplane Model with Single Vertical Tails of Different Size

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Document Details

Document Type
Technical Report
Publication Date
Oct 01, 1943
Accession Number
ADA801045

Entities

People

  • Marvin Pitkin

Organizations

  • Langley Research Center

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Aeronautical Laboratories
  • Air Flow
  • Aircrafts
  • Airplanes
  • Aspect Ratio
  • Blades
  • Coefficients
  • Dihedral Angle
  • Dynamic Pressure
  • Flight
  • Flow
  • Free Flight
  • Fuselages
  • Oscillation
  • Pressure Distribution
  • Propellers
  • Rotation