Attenuation of boundary-layer instabilities for natural laminar flow design on supersonic highly swept wings
Chinese Journal of Aeronautics
2024-07-01
Aufsatz (Zeitschrift)
Elektronische Ressource
Englisch
Natural Laminar Flow Design for Highly Swept Wings
Springer Verlag | 2022
|Swept wings in supersonic flight
TIBKAT | 1954
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