A Survey of Unsteady Hypersonic Flow Problems
A Survey of Unsteady Hypersonic Flow Problems
A Survey of Unsteady Hypersonic Flow Problems
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0<br />
I<br />
From Ref. 29<br />
W as -00, Lid - 3<br />
-0.04 n<br />
0 0.1 0.2 0.3 0.4 Cb-5<br />
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0 Experiment<br />
Inviscid theory<br />
- - -- Theory with two-dimensiona<br />
boundary layer<br />
Effect <strong>of</strong> boundary layer on pressures on circular arc’oglves at M = 6.30