The results of a finite-difference calculation of hypersonic transitional boundary-layer flow are presented. Precursor-transition and low Reynolds number turbulence effects are included. These calculation results are compared with data from a source where profiles are available at the beginning, middle and end of the hypersonic transitional flow. The results indicate that the low Reynolds number effect is the most important.
Calculation of transitional boundary-layer flows.
AIAA Journal ; 11
1973-04-01
Sonstige
Keine Angabe
Englisch
Calculation of transitional boundary-layer flows.
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