TY - GEN
T1 - Shock Wave Boundary Layer Interaction on the STORT Flight Experiment
AU - Willems, Sebastian
AU - Klingenberg, Florian
AU - Hargarten, Dorian
AU - Gülhan, Ali
AU - Plummer, Addison E.
AU - Threadgill, James A.S.
AU - Little, Jesse C.
N1 - Publisher Copyright:
© 2024 by German Aerospace Center (DLR).
PY - 2024
Y1 - 2024
N2 - The German Aerospace Center (DLR) successfully launched a three-stage sounding rocket from the Andøya Space launch site in northern Norway on 26th June 2022. This hypersonic free flight experiment was part of the STORT project and was equipped with several scientific payloads concerning hypersonic technologies. The vehicle performed a suppressed trajectory to increase the integral heat load on the payload, reaching Mach 8 for more than 60 s at an altitude between 30 km and 38 km. Several heat flux and pressure sensors were placed around a canard of the payload to measure the footprint of the shock wave boundary layer interaction (SWBLI). The layout of the experiment as well as the data analysis were done in cooperation with the University of Arizona (UArizona). The design of the experiment and the data analysis were supported with wind tunnel experiments at DLR and the University of Arizona.
AB - The German Aerospace Center (DLR) successfully launched a three-stage sounding rocket from the Andøya Space launch site in northern Norway on 26th June 2022. This hypersonic free flight experiment was part of the STORT project and was equipped with several scientific payloads concerning hypersonic technologies. The vehicle performed a suppressed trajectory to increase the integral heat load on the payload, reaching Mach 8 for more than 60 s at an altitude between 30 km and 38 km. Several heat flux and pressure sensors were placed around a canard of the payload to measure the footprint of the shock wave boundary layer interaction (SWBLI). The layout of the experiment as well as the data analysis were done in cooperation with the University of Arizona (UArizona). The design of the experiment and the data analysis were supported with wind tunnel experiments at DLR and the University of Arizona.
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U2 - 10.2514/6.2024-2384
DO - 10.2514/6.2024-2384
M3 - Conference contribution
AN - SCOPUS:85196159507
SN - 9781624107115
T3 - AIAA SciTech Forum and Exposition, 2024
BT - AIAA SciTech Forum and Exposition, 2024
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA SciTech Forum and Exposition, 2024
Y2 - 8 January 2024 through 12 January 2024
ER -