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Unformatted text preview: and 1.0, compare to the CroccoBusemann relations (both ﬁrst and second). Recall that the CroccoBusemann relations are exact for Pr = 1 . Discuss. How good is the CroccoBusemann approximation for air? Present your results as a brief report. (over) 1 Possible extensions, for extra credit, are as follows. Results should be described in the form of a brief report, to be turned in no later than 30 Nov. 2009. The codes should be emailed as an attachment. 1. Plot the proﬁles as a function of ( y/x ) √ Re x , as in Anderson, HHTG, 2e, Fig. 6.7. 2. Plot the ﬂatplate skinfriction coeﬃcients, as in Anderson, Fig. 6.11. 3. Plot the ﬂatplate Stanton numbers, as in Anderson Fig. 6.12. 4. Compare the exact recovery factors to the simple Blasiusbased theory, as in Anderson Fig. 6.13. 5. Adapt the code to solve for stagnationpoint ﬂow, as in Anderson 2e section 6.5.2. 2...
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 Fall '09
 Fluid Dynamics, Aerodynamics, Ludwig Prandtl, compressible ﬂat plate

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