TY - GEN
T1 - Large Eddy Simulation of Hypersonic Cold Wall Flat Plate-Part II
AU - Kianvashrad, Nadia
AU - Knight, Doyle
N1 - Funding Information:
This research was supported by a grant from the Emil Buehler Foundation and Rutgers Office of Advanced Research Computing for the provision of computational time on Caliburn Supercomputer.
Publisher Copyright:
© 2022, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2022
Y1 - 2022
N2 - In this paper, we evaluate the newly introduced Ht &p method for the prediction of hypersonic flat plate boundary layers. The effects of Mach number and wall temperature are examined as part of the validation. The prediction of Law of Wall, Reynolds Analogy Factor, turbulent Prandtl number, Morkovin, Huang and extended Strong Reynolds Analogy, turbulent shear and normal stresses, power spectrum are in agreement with the theory and available experimental and DNS data. The compressibility effects proved to be significant for the cases examined in this paper.
AB - In this paper, we evaluate the newly introduced Ht &p method for the prediction of hypersonic flat plate boundary layers. The effects of Mach number and wall temperature are examined as part of the validation. The prediction of Law of Wall, Reynolds Analogy Factor, turbulent Prandtl number, Morkovin, Huang and extended Strong Reynolds Analogy, turbulent shear and normal stresses, power spectrum are in agreement with the theory and available experimental and DNS data. The compressibility effects proved to be significant for the cases examined in this paper.
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U2 - 10.2514/6.2022-0588
DO - 10.2514/6.2022-0588
M3 - Conference contribution
AN - SCOPUS:85123220780
SN - 9781624106316
T3 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
BT - AIAA SciTech Forum 2022
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - AIAA Science and Technology Forum and Exposition, AIAA SciTech Forum 2022
Y2 - 3 January 2022 through 7 January 2022
ER -