QUESTION 14 The fan of a turbofan engine is tested at high speed. The flow approaches the fan tip at a relative Mach num

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QUESTION 14 The fan of a turbofan engine is tested at high speed. The flow approaches the fan tip at a relative Mach num

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Question 14 The Fan Of A Turbofan Engine Is Tested At High Speed The Flow Approaches The Fan Tip At A Relative Mach Num 1
Question 14 The Fan Of A Turbofan Engine Is Tested At High Speed The Flow Approaches The Fan Tip At A Relative Mach Num 1 (57.86 KiB) Viewed 36 times
QUESTION 14 The fan of a turbofan engine is tested at high speed. The flow approaches the fan tip at a relative Mach number M1rel = 1.19. An oblique shock forms at the fan tip leading edge, with a shock angle B = 87 degrees. Use cold-air- standard assumptions and the two-dimensional oblique shock formulae to determine the relative Mach number M2rel after the shock. State your answer to two decimal places. Partial credit is awarded for a reasonable approximation to the correct numerical answer.
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