A New Flow-Through Wind Tunnel Balance Concept for Retropropulsion Testing

von Burns, Devin E.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Fluid dynamics ; Volume 4 of 7 (2022)

ARTIFICIAL THICKENING OF A TRANSONIC BOUNDARY LAYER IN THE PRESENCE OF A PRESSURE GRADIENT ASSOCIATED WITH A BOUNDARY LAYER INGESTION CONCEPT

von Jones, Gregory S.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 1 of 7 (2020)