Accession Number : ADP005019

Title :   Wind Tunnel and Flight Test Analysis and Evaluation of the Buffet Phenomena for the Alpha Jet Transonic Wing,

Corporate Author : DORNIER SYSTEM G M B H FRIEDRICHSHAFEN (GERMANY F R)

Personal Author(s) : Buers,H. ; Schmitt,V.

Report Date : NOV 1985

Pagination or Media Count : 11

Abstract : Results of local flow surveys on the wing in the buffeting region are presented. The vibration levels on the wing and at the pilot's seat are also shown. The paper presents the separated effects of the slats in use both with and without trailing edge flaps as manoeuvre flaps up to the transonic flight regime.

Descriptors :   *TRANSONIC AIRFOILS, *BUFFETING, WINGS, VIBRATION, BOUNDARY LAYER FLOW, FLOW SEPARATION, TRAILING CONTROL SURFACES, FLAPS(CONTROL SURFACES), TRANSONIC FLIGHT, JET AIRCRAFT, WIND TUNNEL TESTS, MATHEMATICAL PREDICTION, FRANCE, WEST GERMANY

Distribution Statement : APPROVED FOR PUBLIC RELEASE