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IDEAL FLUIDS 1 The equation of continuity
2 Eulers equation
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according adiabatic angle appear axis becomes body boundary boundary conditions boundary layer calculation called characteristics co-ordinates coefficient compared complete component condition conduction consider constant continuity corresponding course cross-section decreases denote density depends derivative determined dimension direction discontinuity distance distribution drag effect energy entropy equal equation equilibrium expression Finally flow fluid flux follows force formula frequency function given gives grad heat Hence incident increases infinite initial integral lift force limiting mass mean momentum moves normal obtain occurs oscillations past perturbations pipe plane positive potential pressure PROBLEM propagated properties quantities regarded region relation relative respect rest result Reynolds number satisfied separation shock wave side similar simple solution sound sound wave sphere steady streamlines Substituting suppose surface taken temperature thermal turbulent unit varies vector viscosity volume wake write zero