An Application of CFD to Guide Forced Boundary-Layer Transition for Low-Speed Tests of a Hybrid Wing-Body Configuration (AIAA 2016-3981)
32nd AIAA aerodynamic measurement technology and ground testing conference 2016 ; 2016 ; Washington D.C
2016-01-01
23 pages
Conference paper
English
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Airframe Noise from a Hybrid Wing Body Aircraft Configuration (AIAA 2016-2708)
British Library Conference Proceedings | 2016
|DataCite | 1921
British Library Conference Proceedings | 2016
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