USM3D ANALYSES IN SUPPORT OF THE NASA LANGLEY 0.3-METER TRANSONIC CRYOGENIC TUNNEL TEST OF BOUNDARY-LAYER THICKENER CONFIGURATIONS

von Bozeman, Michael D.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Fluid dynamics ; Volume 7 of 7 (2020)

Evaluation of Limiter Functions for Supersonic Applications

von Ahmad, Nashat N.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 5 of 5 (2023)

USM3D SIMULATIONS FOR THIRD SONIC BOOM WORKSHOP

von Elmiligui, Alaa A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Inlets, nozzles, and propulsion systems integration (2021)

USM3D SIMULATIONS FOR THIRD SONIC BOOM WORKSHOP

von Elmiligui, Alaa A.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Applied aerodynamics ; Volume 2 of 5 (2021)

X-59 Air Data Probe Calibration Wind Tunnel Test

von Winski, Courtney S.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 5 of 5 (2023)

Measurement Accuracy and Uncertainty Analysis of the X-59 Air Data Probe Calibration Test Entry One

von Friedlander, David J.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 5 of 5 (2023)

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)

X-59 Sonic Boom Test Results from the NASA Glenn 8- By 6-Foot Supersonic Wind Tunnel

von Durston, Donald A.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Applied aerodynamics ; Volume 5 of 5 (2023)

X-59 Sonic Boom Test Results from the NASA Glenn 8- By 6-Foot Supersonic Wind Tunnel

von Durston, Donald A.
Veröffentlicht in AIAA Aviation Forum (2023 : San Diego, Calif.; Online) Supersonics (2023)