Publikationsdatum:
2011-08-24
Beschreibung:
Computations were made for those test cases of Problem 3 which were designated as laminar flows, viz., test cases 3.1, 3.2, 3.4, and 3.5. These test cases corresponded to flows over a flat plate and a compression ramp at high Mach number and at high Reynolds number. The computations over the compression ramps indicate a substantial streamwise extent of separation. Based on previous experience with separated laminar flows at high Mach numbers which indicated a substantial effect with spatial grid refinement, a series of computations with different grid sizes were performed. Also, for the flat plate, comparisons of the results for two different algorithms were made.
Schlagwort(e):
AERODYNAMICS
Materialart:
In: Hypersonic flows for reentry problems. Vol. 2 (A93-42576 17-02); p. 244-254.
Format:
text
