Reynolds number and wall cooling effects on correlations between the thermodynamic variables in hypersonic turbulent boundary layers
The Reynolds number and wall cooling effects on correlations between the thermodynamic
variables are systematically investigated in hypersonic turbulent boundary layers by direct …
variables are systematically investigated in hypersonic turbulent boundary layers by direct …
Spectra scaling of velocity components and pressure–strain correlations for hypersonic boundary layers at a range of wall-to-recovery temperatures
W Liu, R Huang, J Wu - Physics of Fluids, 2023 - pubs.aip.org
Flow similarity is one of the most desirable features for turbulence under different conditions.
For hypersonic boundary layers, different wall temperatures are known to change the …
For hypersonic boundary layers, different wall temperatures are known to change the …
Heat-transfer effects in compressible turbulent boundary layers–a regime diagram
As shown by Wenzel et al.(J. Fluid Mech., vol. 930, 2022, A1), the Eckert number can be
determined in advance–or estimated to a reasonable extent–a key advantage of the …
determined in advance–or estimated to a reasonable extent–a key advantage of the …
[PDF][PDF] Heat transfer effects in compressible turbulent
As shown by Wenzel et al.(2022) the Eckert number defined as 𝐸𝑐= 𝑢2 𝑒/(𝑐𝑝 (𝑇𝑟− 𝑇𝑤))=
7 (𝛾− 1) 𝑀2 𝑒𝑇𝑒/(𝑇𝑟− 𝑇𝑤) can be understood as a meaningful quantity to compare heat-8 …
7 (𝛾− 1) 𝑀2 𝑒𝑇𝑒/(𝑇𝑟− 𝑇𝑤) can be understood as a meaningful quantity to compare heat-8 …