Validation Of Comprehensive Modeling Of The Wing And Rotor Aeroelastic Test System
72nd American Helicopter Society International Annual Forum 2016 ; 2016 ; West Palm Beach, Florida
01.01.2016
17 pages
Aufsatz (Konferenz)
Englisch
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
British Library Conference Proceedings | 2018
|Rotor wing integral vibration mode excitation method for rotor wing aeroelastic stability test
Europäisches Patentamt | 2021
|Validation of an Aeroelastic Rotor Analysis Method
AIAA | 2018
|