TY - GEN
T1 - Considerations for a hypersonic flight test investigating fluid-thermal-structural interactions
AU - McQuellin, Liam P.
AU - Neely, Andrew J.
AU - Currao, Gaetano M.D.
N1 - Funding Information:
This material is based upon ground-test work on high-speed FSI supported by the Air Force Office of Scientific Research under award number FA2386-19-1-4027 and the Australian Research Council under ARC-DP180103480.
Publisher Copyright:
© 2020, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2020
Y1 - 2020
N2 - This study presents design considerations for a hypersonic flight test, where a primary or tertiary payload includes a single or multiple experiments to explore fluid-thermal-structural-interactions. This multi-physics problem remains a state-of-the-art research area, with greater emphasis being placed on understanding its role on the performance and survivability of hypersonic vehicles. This paper provides an overview of fluid-thermal-structural-interactions in hypersonic flight, and presents the current approaches being employed to further understand the problem. The need for a dedicated flight test is discussed, and measured against achievements that could be produced through successive tertiary experiments on flight tests focusing on other problems. Previous methods to instrument hypersonic flight-tests are examined, and potential methods to instrument an FTSI focused test are proposed.
AB - This study presents design considerations for a hypersonic flight test, where a primary or tertiary payload includes a single or multiple experiments to explore fluid-thermal-structural-interactions. This multi-physics problem remains a state-of-the-art research area, with greater emphasis being placed on understanding its role on the performance and survivability of hypersonic vehicles. This paper provides an overview of fluid-thermal-structural-interactions in hypersonic flight, and presents the current approaches being employed to further understand the problem. The need for a dedicated flight test is discussed, and measured against achievements that could be produced through successive tertiary experiments on flight tests focusing on other problems. Previous methods to instrument hypersonic flight-tests are examined, and potential methods to instrument an FTSI focused test are proposed.
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U2 - 10.2514/6.2020-2419
DO - 10.2514/6.2020-2419
M3 - Conference contribution
AN - SCOPUS:85087902499
SN - 9781624106002
T3 - 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020
BT - 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 23rd AIAA International Space Planes and Hypersonic Systems and Technologies Conference, 2020
Y2 - 10 March 2020 through 12 March 2020
ER -