Numerical Analysis to Evaluate the Effect of Wall Temperature on Skin Friction and Stanton Number for Turbulent Flows over a Flat Plate from Mach 2–8

Pasha, Amjad Ali; Reddy, D. Siva Krishna; Abdulla, M. M.; Pillai, S. Nadaraja; Islam, Nazrul; Juhany, Khalid A.; Reddy, V. Mahendra; Jameel, Abdul Gani Abdul

doi:10.1007/s13369-021-06170-w

Arab J Sci Eng

2021

DOI: 10.1007/s13369-021-06170-w

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Numerical Analysis to Evaluate the Effect of Wall Temperature on Skin Friction and Stanton Number for Turbulent Flows over a Flat Plate from Mach 2–8

Amjad Ali Pasha

D. Siva Krishna Reddy

M. M. Abdulla

et al.

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Analysis of the wall heat flux of the hypersonic shock wave/boundary layer interaction using a novel decomposition formula

Sun,

Liu,

et al. 2024

Theor. Comput. Fluid Dyn.

View full text Add to dashboard Cite

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Numerical Analysis to Evaluate the Effect of Wall Temperature on Skin Friction and Stanton Number for Turbulent Flows over a Flat Plate from Mach 2–8

Cited by 1 publication

References 45 publications

Analysis of the wall heat flux of the hypersonic shock wave/boundary layer interaction using a novel decomposition formula

Analysis of the wall heat flux of the hypersonic shock wave/boundary layer interaction using a novel decomposition formula

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