Unsteady Optimization Using a Discrete Adjoint Approach Applied to Aeroacoustic Shape Design
46th AIAA Aerospace Sciences Meeting and Exhibit
01.01.2008
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Unsteady Optimization Using a Discrete Adjoint Approach Applied to Aeroacoustic Shape Design
British Library Conference Proceedings | 2008
|UNSTEADY ADJOINT METHOD FOR AEROACOUSTIC PROPELLER OPTIMIZATION
TIBKAT | 2021
|