
The reservoir of a supersonic windtunnel has a total temperature and total pressure of \(600\,K\) and \(11\,atm\). If the flow …
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Find the enthalpy change, internal energy change and entropy change across a shock wave whose upstream air temperature and pressure …
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Find the neutral point and static margin of an airplane if the location of the aerodynamic center is at \( …
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Consider wing body combination of an airplane. Find the coefficient of lift of this wing body if the coefficient of …
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Find the turn radius and turn rate of an airplane, flying at a velocity of \(403.2\, km/h\) and has a …
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Find the stalling speed of an airplane which has a wing area of \(17\,m^2\) and is flying at sea level …
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The velocity at a point on the wing placed in a wind tunnel is \(251 m/s\). The pressure and temperature …
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Find the coefficient of pressure at a point on the wing where the velocity is \(58\,m/s\). The airplane is flying …
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Calculate the pressure coefficient at a point on the airfoil where the pressure is \( 8.9 \times 10^4\,N/m^2\). Airfoil is …
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Calculate the lift, drag and moment coefficient about quarter chord per unit span of an airfoil which is at an …
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