S.L. Liguore, D.M. Pitt

Modern aircraft have become faster and more agile, and consequently, are flying more often in conditions of separated flow. The wing experiences buffeting response under conditions of separated flow. The structural loads caused by buffeting are important design limit load and fatigue load conditions. Under these demanding flight environments, severe buffet can drastically reduce the fatigue life of the airframe. New aircraft development programs require the earliest definition of these buffet loads in the structural sizing of aircraft.

International Forum on Aeroelasticity and Structural Dynamics, 2005, München

Conference Paper

englisch

21,0 x 29,7 cm, 12 Seiten

DGLR-Bericht, 2005, 2005-04, International Forum on Aeroelasticity and Structural Dynamics 2005; S.1-12; 2005; Deutsche Gesellschaft für Luft- und Raumfahrt - Lilienthal-Oberth e.V., Bonn

NA

in getr. Zählung;

loads (forces), wind tunnel tests, unsteady aerodynamics, buffet

Bibliothek

2005