PTERODACTYL: AERODYNAMIC AND AEROHEATING MODEL FOR A SYMMETRIC DEPLOYABLE ENTRY VEHICLE WITH FLAPS

von Reddish, Brandon
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Guidance, navigation, and control ; Volume 2 of 4 (2021)

Pterodactyl: Thermal Protection System Design Methodology for a Flap Control System

von Hays, Zane B.
Veröffentlicht in AIAA SciTech Forum and Exposition (2022 : San Diego, Calif.; Online) Atmospheric flight mechanics ; Volume 1 of 2 (2022)

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)

MODEL DESIGN AND PRE-TEST CFD ANALYSIS FOR A SUPERSONIC RETROPROPULSION WIND TUNNEL TEST

von Edquist, Karl T.
Veröffentlicht in AIAA SciTech Forum and Exposition (2020 : Orlando, Fla.) Applied aerodynamics ; Volume 4 of 4 (2020)

FLOW CHARACTERIZATION OF THE NASA LANGLEY UNITARY PLAN WIND TUNNEL, TEST SECTION 2: COMPUTATIONAL RESULTS

von Childs, Robert
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Ground testing (2021)

PTERODACTYL: SYSTEM ANALYSIS OF AN ASYMMETRIC AND SYMMETRIC DEPLOYABLE ENTRY VEHICLE FOR PRECISION TARGETING USING FLAPS

von D'Souza, Sarah N.
Veröffentlicht in AIAA SciTech Forum and Exposition (2021 : Online) Guidance, navigation, and control ; Volume 2 of 4 (2021)

EVALUATION OF CFD FOR SIMULATION OF HIGH-SUPERSONIC CONTROL-SURFACE EFFECTIVENESS

von Ross, James C.
Veröffentlicht in AIAA Aviation Forum (2021 : Online) Ground testing (2021)