V/STOL Aircraft Aerodynamic Prediction Methods Investigation. Volume 3. Manual for Computer Programs

Abstract

Analytical engineering methods are developed for use in predicting the static and dynamic stability and control derivatives and force and moment coefficients of lift-jet, lift-fan, and vectored thrust V/STOL aircraft in the hover and transition flight regimes. The aircraft configurations studies have a conventional wing, fuselage and empennage. The prediction methods are suitable for use by design personnel during the preliminary design and evaluation of V/STOL aircraft of the type previously mentioned. Details and listings of the computer programs associated with the prediction methods are given in the volume.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1972
Accession Number
AD0752559

Entities

People

  • Henry Ziegler
  • Howard R. Wasson
  • Hsiao C. Kao
  • Myles F. Schwendemann
  • Peter T. Wooler

Tags

Communities of Interest

  • Air Platforms
  • Energy and Power Technologies

DTIC Thesaurus Topics

  • Air Force
  • Aircraft Equipment
  • Aircraft Wings
  • Aircrafts
  • Computational Science
  • Computer Programming
  • Computer Programs
  • Computers
  • Coordinate Systems
  • Flight
  • Flow
  • Geometry
  • Molecular Dynamics
  • Pressure Distribution
  • Self Assembly
  • Short Takeoff Aircraft
  • Three Dimensional

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Aerospace Engineering
  • Business Analytics