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).

the equation above shows how temperature f, measured in degrees fahrenheit, relates to a temperature c, measured in degrees celsius. based on the equation, which of the following must be true?

a temperature increase of 1 degree fahrenheit is equivalent to a temperature increase of

5

9

degree celsius.

a temperature increase of 1 degree celsius is equivalent to a temperature increase of 1.8 degrees fahrenheit.

a temperature increase of

5

9

degree fahrenheit is equivalent to a temperature increase of 1 degree celsius.

a) i only

b) ii only

c) iii only

d) i and ii only

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