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Why is critical Mach number of a sphere higher than a cylinder ?
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Velocity potential of a subsonic compressible flow is \[\phi(x,y) = V_{\infty}x + \frac{5}{\sqrt{1 – M_{\infty}^{2}}}e^{-2\pi\sqrt{1-M_{\infty}^{2}}y}sin2\pi x\] Freestream velocity, pressure and …
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An airfoil is in airflow with \(0.52\) free stream Mach number. Local Mach number at a given point is \(0.83\). …
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How urban air mobility work?
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What is AWACS?
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What is the difference between inertial navigation system (INS) and inertial reference system (IRS) in aviation?
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How air traffic control helps in communication, navigation and surveillance of the aircrafts?
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What are the instruments that are present inside an aircraft’s cockpit?
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What are form drag and profile drag ?
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What is a Jet lag ?
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