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As compare to turbo- prop, a turbo- jet

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A typical value of this critical Mach number is of the order of

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Under which one of the following sets of conditions will a supersonic compressor have the highest efficiency?

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The flight mach number of the aircraft is

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In normal shock in a gas, the

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The prime parameter causing change of state in a Fanno flow is

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In the case of Fanno line flow, in the subsonic region friction causes

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Compared to a turbo- jet engine, a turbo- prop engine has a higher power for take – off

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Rayleight line flow is a flow in a constant area duct

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Fanno line flow is a flow in a constant area duct

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Consider the following statements about a rocket engine:

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For oblique shock, the downstream mach number

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Across the normal shock, the fluid properties change in such a manner that the

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Only rocket engines can be propelled to space because

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Consider the following statements relating to rocket engines:

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In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output

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In a turbo- jet engine, subsequent to heat addition to compressed air, to get the power output

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In open cycle turbo- jet engines used in

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In the subsonic range the propulsive efficiency of a rocket less than

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The propulsive efficiency of the units is

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