Wind Tunnel Investigation of Varying Hinged Flaps.

Abstract

The objective of this thesis was to compare thin-airfoil theoretical predictions of the change in zero-lift angle of attack divided by flap deflection versus flap-hinge location and the change in moment coefficient about the aerodynamic center.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1982
Accession Number
ADA124703

Entities

People

  • Howard J. Price Jr

Organizations

  • Air Force Institute of Technology

Tags

Communities of Interest

  • Ground and Sea Platforms

DTIC Thesaurus Topics

  • Air Force
  • Coefficients
  • Computer Programs
  • Computers
  • Coordinate Systems
  • Crystal Structure
  • Data Reduction
  • Deflection
  • Dynamic Pressure
  • Engineering
  • Experimental Data
  • Flow
  • Free Stream
  • Measurement
  • Three Dimensional
  • Two Dimensional
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.