Effect of an Unswept Wing on the Contribution of Unswept-Tail Configurations to the Low-Speed Static- and Rolling-Stability Derivatives of a Midwing Airplane Model

Abstract

An investigation has been conducted in the Langley stability tunnel to determine the effect of an unswept wing on the contribution of unswept-tail configurations to the low-speed static and rolling-stability derivatives of a midwing airplane model.

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Document Details

Document Type
Technical Report
Publication Date
Aug 01, 1950
Accession Number
ADA380554

Entities

People

  • Donald R. Riley
  • William Letko

Organizations

  • National Aeronautics and Space Administration

Tags

Communities of Interest

  • Air Platforms

DTIC Thesaurus Topics

  • Accuracy
  • Aerodynamic Characteristics
  • Aerodynamic Configurations
  • Aeronautical Laboratories
  • Air Force
  • Air Force Facilities
  • Aircrafts
  • Airfoils
  • Airplanes
  • Aspect Ratio
  • Dynamic Pressure
  • Flow
  • High Angles
  • Horizontal Stabilizers
  • Low Angles
  • Measurement
  • Wing Tips

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.