AIAA-2019-3388: Aeroelastic Indicial Response Reduced-Order Modeling for Flexible Flight Vehicles
Applied aerodynamics ; 2019 ; Dallas, TX
01.01.2019
32 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
DataCite | 1910
Static Aeroelastic Effects on a Transonic Indicial Response Wing Flutter Calculation
Online Contents | 1998
|