Accession Number : ADA299463
Title : Flight Flutter Test of a Nomad N24A Aircraft Fitted with One Modified Aileron.
Descriptive Note : Technical note,
Corporate Author : DEFENCE SCIENCE AND TECHNOLOGY ORGANIZATION CANBERRA (AUSTRALIA)
Personal Author(s) : Farrell, P. A. ; Dunn, S. A.
PDF Url : ADA299463
Report Date : JUN 1995
Pagination or Media Count : 37
Abstract : A Nomad aileron was modified by the addition of strain gauges and associated wiring, to permit its use in loads-measurement trials. This modification rendered the aileron non-standard, so a flight flutter trial was conducted to verify the aeroelastic stability of the loads aircraft when fitted with this aileron. This report describes the flight flutter trial and presents the results.
Descriptors : *FLUTTER, *AILERONS, FLIGHT TESTING, STABILITY, AEROELASTICITY, STRAIN GAGES.
Subject Categories : Aircraft
Distribution Statement : APPROVED FOR PUBLIC RELEASE