Aircraft System Noise Prediction Uncertainty Quantification for a Hybrid Wing Body Subsonic Transport Concept
2018 AIAA/CEAS Aeroacoustics Conference
01.01.2018
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
British Library Conference Proceedings | 2018
|Wing/Fuselage Structural Concept Study for a Subsonic Transport Aircraft
SAE Technical Papers | 1973
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