Accession Number : ADA131033

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

Descriptive Note : Aerodynamics technical memo.,

Corporate Author : AERONAUTICAL RESEARCH LABS MELBOURNE (AUSTRALIA)

Personal Author(s) : Ludowyk,C J

PDF Url : ADA131033

Report Date : Jan 1983

Pagination or Media Count : 49

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.

Descriptors :   *Gust loads, Aerodynamic stability, Utility aircraft, Aircraft models, Roll, Pitch(Motion), Transfer functions, Aerodynamic forces, Australia

Subject Categories : Transport Aircraft
      Fluid Mechanics

Distribution Statement : APPROVED FOR PUBLIC RELEASE