An Application of CFD to Guide Forced Boundary-Layer Transition for Low-Speed Tests of a Hybrid Wing-Body Configuration
32nd AIAA Aerodynamic Measurement Technology and Ground Testing Conference
2016-01-01
Conference paper
Electronic Resource
English
British Library Conference Proceedings | 2016
|Boundary-Layer Transition on a Forward-Swept Wing in Canard Configuration
Online Contents | 1996
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