C. Reschke, G. Looye

Two approaches for the development of aircraft models integrating flight and airframe structural dynamics are compared. These models are intended for flight loads analysis and flight simulator application. The approaches combine available, agreed on flight mechanics and aeroelastic aircraft models from the respective engineering disciplines. The present work compares two methods, with different underlying assumptions, regarding accuracy, implementability, pre-processing and computing effort, as well as possibility to adapt the model components as a function of the flight condition.

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;

simulation, aeroelasticity, flight mechanics, models, integration

Bibliothek

2005