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1.2250 <br />
<br />
Additionally, must be represented in consistent units,<br />
350 <br />
1000<br />
1<br />
<br />
1 3600 <br />
97.2 <br />
<br />
Using the equation derived in the analysis, the required thrust is given by,<br />
Note that,<br />
1 <br />
1.2250<br />
2 97.2<br />
<br />
<br />
· <br />
<br />
4739.4 436.04<br />
· <br />
5175.4 <br />
27.3 0.03 <br />
1 1<br />
238220 <br />
1.2250 <br />
97.2<br />
27.30.97.5 · <br />
<br />
For part (b), it is first necessary to find the air density at 4.5 . From Appendix A,<br />
0.77704 <br />
<br />
Using the equation derived in the analysis, the required thrust is given by,<br />
1<br />
<br />
0.77704<br />
2 97.2<br />
<br />
<br />
· <br />
<br />
3006.3 687.42<br />
· <br />
3693.7 <br />
27.3 0.03 <br />
238220 <br />
0.77704 <br />
97.2<br />
27.30.97.5
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