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The thrust F developed by a rocket motor is given by F = mv +A(P 1 -P 2 ), where m is the mass of fuel ejected per unit time ,V is the velocity of the ejected gas ,A is the area of the nozzle,P 1 and P 2 are the pressures. Show that the equation given is dimensionally correct.
Dear Karan F = [M L T-2] mv = [M T-1] [L T-1] = [M L T-2] A(P1 – P2) = AP = [L2] [M L-1 T-2] = [M L T-2] Hence verified
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