Gust Response of a Light, Single-Engined, High-Wing Aircraft.

Abstract

A recently developed Fortran program for calculating rigid-aircraft gust response has been applied to obtain Longitudinal and Lateral transfer functions and output response spectra for a general aviation, high-wing aircraft.

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Document Details

Document Type
Technical Report
Publication Date
Jan 01, 1983
Accession Number
ADA131033

Entities

People

  • C. J. Ludowyk

Tags

DTIC Thesaurus Topics

  • Aerodynamic Characteristics
  • Aerodynamics
  • Air Force
  • Aircrafts
  • Control Systems
  • Department Of Defense
  • Engineering
  • Frequency Response
  • Horizontal Stabilizers
  • Mechanical Engineering
  • Moment Of Inertia
  • Production Engineering
  • Spectra
  • Stabilized Platforms
  • Standards
  • Transfer Functions
  • Wind Tunnels

Fields of Study

  • Physics

Readers

  • Aerodynamics/Aeronautics.
  • Computer Science.