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
Distribution Statement : APPROVED FOR PUBLIC RELEASE