Three-Dimensional Flowfield Measurements of a Swept-back Cantilevered Wing at High Angles of Attack
AIAA SCITECH 2022 Forum
01.01.2022
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
Flowfield of a swept blade tip at high pitch angles
AIAA | 1991
|Plasma Control of Flow Separation on Swept Wing at High Angles of Attack
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