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Find the inlet area of a ramjet engine, if the maximum thrust to be produced is \(5000\, N\) at sea …
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An airplane is flying at an altitude of \(10,000\,m\) with a turbojet engine at a velocity of \(900\, km/h\). The …
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- 1 answers
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What is the working principle of a turbojet engine ?
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What is thrust reversal ? What are the methods of thrust reversal ?
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What are the advantages of a turbojet engine ?
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The temperature distribution at a certain input of time in concrete slab during curing is given by \(T=3x^{2}+3x+16\) where \(x\) …
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The temperature field in a body varies according to the equation \(T(x,y)=x^{3}+4xy\).Find the direction of fastest variation in temperature at …
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In case of ideal triatomic gas , What is the ratio of specific heats \(C_p/C_v\)?
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A jet engine is operating at a Mach number of \(0.8\) at an altitude of \(10 \;km\).The efficiency of the …
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A turbojet powered aircraft is flying at Mach number \(0.8 \) at an altitude of \(10\; km\).The inlet and exit …
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- 0 votes
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Find the location of the aerodynamic center.
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Find the angle of attack for this airfoil, if the lift per unit span produced is \(1400\,N\).
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Can an airfoil fly upside-down ?
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Find the circulation around a spinning circular cylinder in free stream flow of velocity \(40\,m/s\) at a standard sea level conditions, if the lift produced by the cylinder is \(8\,N/m\) of span.
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An airplane is flying at an velocity of \(100\,m/s\). Find the pressure coefficient at a point on the surface of the wing where the flow velocity is \(140\,m/s\).
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