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A Survey of Unsteady Hypersonic Flow Problems

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- 24 -<br />

minimum are that its variations for small variations in the values <strong>of</strong> p, q<br />

and $ should be zero. These conditions can be shown to lead to the equations<br />

<strong>of</strong> continuity, irrotationality and momentum for the flow, so that the problem<br />

<strong>of</strong> finding the flow by solving the equations <strong>of</strong> motion for the fluid can be<br />

change& into that <strong>of</strong> finding a function for p which makes the integral in<br />

equation (2.42) a minimum.<br />

For isentropic conditions, p can be expressed in terms <strong>of</strong> the<br />

velocity potential, 6, in the form<br />

p = r, (y-l) ( f! + $o(y-')<br />

. . . ( 2 . 4 3 )<br />

Ibo L<br />

where s, is the free-stream<br />

can be written in the form<br />

ta<br />

PC.3 I<br />

t; ‘J(t) ti lb (t) [<br />

& Iat /-I<br />

speed <strong>of</strong> sound. Using this expression, equation (2.42)<br />

-!I$(;+ $$)~y-r)w a, (2.44)<br />

and the problem becomes that <strong>of</strong> finding a function for $ such that the variation<br />

in I is sero for small variations in +. This problem canbe solved in an<br />

approximate manner by assuming a finite series for 4 which satisfies the boundary<br />

conditions (including the known conditions at k and I+) and in which the<br />

coefficients are determined by the condition that the variation in I for small<br />

variations in each coefficient must be sero.<br />

When this general method is applied to the case <strong>of</strong> flow around a<br />

two-dimensional piston in Ref. 19 it is shown that the statement <strong>of</strong> the variational<br />

principle must be modified slightly to take account <strong>of</strong> the fact that the conditions<br />

at time te are not known. The modified statement has the form<br />

A][(; dv at +~t2;pA~lt~t2~~ = 0 . . . (2.45)<br />

+a<br />

where A p dV dt is the small variation in the integral for a small variation<br />

h u(t)<br />

in P (or +), and A+ is the corresponding small variation in +. The variations<br />

must be taken so that A$ = 0 at the outer wave from the piston, the boundary<br />

conditions at the piston are unaltered, and at time b the disturbed volume is<br />

zero or the flm is known everywhere and the variations are correspondingly<br />

restrained. When both p and p are expressed in terms <strong>of</strong> the velocity potential<br />

equation (2.45) can be written as:<br />

where S(t) is the disturbed area in the two-dimensional problem.<br />

. . . (2.46)<br />

Zartari*n19/

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