

MCQOPTIONS
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1. |
Calculate the approximate value of length at which supersonic after burning engine could be design in such a way that thrust at takeoff will be 29800 unit and maximum Mach number will be 2.12. |
A. | 219 |
B. | 100 |
C. | 301 |
D. | 183.129 |
Answer» B. 100 | |