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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Dcfmitions <strong>of</strong> derivatives<br />
"B<br />
L, = -<br />
& = Ee - 4kaeg')<br />
2k=<br />
La =& for piston theory<br />
"B<br />
k = -k<br />
~ _ _ (me - 4ka$<br />
k=<br />
Ma = kb for piston theory<br />
2m6<br />
& = -k<br />
where Lift = 4p, U, b k2euut<br />
. r<br />
and pitching moment = -4+%J~ bakae<br />
- 68 -<br />
iwt h<br />
[ - 04 + NJ') + %(M, + w<br />
b I<br />
The quantities L&, G, &, Mi, &, & refer to the leading-edge axis (x0 = 0).<br />
Aclmowledgements<br />
The author wishes to acknowledge the help received in the preparation<br />
<strong>of</strong> this report from discussions with colleagues at the National Physical<br />
Laboratory. He wishes to acknowledge with particular gratitude the help,<br />
advice and encouragement received from Mr. N. C. Lamboume.<br />
References/