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Engineering, 26.07.2019 16:10 salazjlove

Aramjet engine provides thrust at 12.8 km altitude. the stagnation temperature at the inlet of the nozzle is 2030°c. sketch the variation of thrust force with respect to the flight mach number. (ra=0.32, rc=0.9, rn=0.9, p, = p6=0.2 atm, t = -51°c, no=0.99, qr=43 mj/kg, ac= 0.04 m²).

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Aramjet engine provides thrust at 12.8 km altitude. the stagnation temperature at the inlet of the n...
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