TY - GEN
T1 - Stability Analysis of Hypervelocity Ballistic-Range Data
AU - Hameed, A.
AU - Chen, J. H.
AU - Parziale, N. J.
AU - Dungan, S.
AU - Saikia, B.
AU - Brehm, C.
N1 - Publisher Copyright:
© 2023, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2023
Y1 - 2023
N2 - This paper analyzes hypervelocity ballistic-range transition experiments performed by Sheetz using the STABL and CHAMPS stability techniques. Comparison between the two computational techniques is performed for two experiments and the stability calculations are found to be nominally consistent. In the experiments where the second mode should dominate transition, the N-factor of transition was found to be higher than that in a conventional hypersonic facility. An assessment was conducted of the spread of the N-factor at the transition location for a subset of experiments where the geometry and physics governing transition should be the same. Conventional transition location correlations are presented and, although they are not mechanism based, the correlations do appear to separate the data into distinct groupings which can inform further mechanism-based analysis.
AB - This paper analyzes hypervelocity ballistic-range transition experiments performed by Sheetz using the STABL and CHAMPS stability techniques. Comparison between the two computational techniques is performed for two experiments and the stability calculations are found to be nominally consistent. In the experiments where the second mode should dominate transition, the N-factor of transition was found to be higher than that in a conventional hypersonic facility. An assessment was conducted of the spread of the N-factor at the transition location for a subset of experiments where the geometry and physics governing transition should be the same. Conventional transition location correlations are presented and, although they are not mechanism based, the correlations do appear to separate the data into distinct groupings which can inform further mechanism-based analysis.
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U2 - 10.2514/6.2023-3705
DO - 10.2514/6.2023-3705
M3 - Conference contribution
AN - SCOPUS:85200243235
SN - 9781624107047
T3 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
BT - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
T2 - AIAA Aviation and Aeronautics Forum and Exposition, AIAA AVIATION Forum 2023
Y2 - 12 June 2023 through 16 June 2023
ER -