5 and an upstream stagnation pressure of 5

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Unformatted text preview: '58#/$),$8"#$)*-#8$5'#5$)3$K:P$26:$ Calculate the thrust, if the inlet area is 0.5 m2 . $ U ! ! " # $ 3. To compensate for Anderson’s leaving out an important column in the isentropic flow table, A write a Matlab script that tabulates the quantity pp0 A∗ . Your script should read in a value for γ , a starting and ending value for M , and a step by which to increment M . It should A then print out a table of two columns, M and pp0 A∗ . Using Anderson’s tables, and your new Matlab scr...
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This note was uploaded on 04/14/2010 for the course AEROSP 225 taught by Professor Powell during the Winter '10 term at University of Michigan.

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