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IDEAL FLUIDS 1 The equation of continuity
2 Eulers equation
133 other sections not shown
adiabatic amplitude angle axis Bernoulli's equation body boundary conditions boundary layer calculation characteristics co-ordinates coefficient combustion constant corresponding cross-section cylindrical denote derivative determined detonation wave dimension direction distance drag drag coefficient energy flux entropy equation of continuity equations of motion equilibrium Euler-Tricomi equation Euler's equation expression finite flow past fluid velocity flux density formula frequency function gas velocity given gives grad gradient heat helium Hence incident incompressible increases infinite infinity integral intersection laminar Laplace's equation lift force mean mechanical equilibrium moving obtain occurs oscillations parameters particles perturbations pipe plane potential flow pressure Problem propagation quantities radius rarefaction wave result Reynolds number shock wave small compared solution sound wave sphere spherical streamlines subsonic Substituting superfluid supersonic surface of discontinuity tensor thermal conduction thermodynamic turbulent flow turbulent region vector velocity component velocity of sound viscosity volume wake weak discontinuity zero