## Gas Dynamics |

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### Contents

Basic Equations of Compressible Flow | 1 |

Wave Propagation in Compressible Media | 23 |

Varying Area Channel 3 4 Stagnation Properties | 48 |

Copyright | |

16 other sections not shown

### Common terms and phrases

adiabatic airfoil angle of attack Appendix Assume back pressure boundary conditions boundary layer calculate Chapter characteristics choked compressible flow cone constant specific heats constant-area control volume converging-diverging nozzle curve decrease density derived determine diffuser electric energy equation entropy equal equations of motion example expansion waves Fanno flow flow direction ft/sec Gas Dynamics gas flow gas with constant gases heat addition heat transfer incompressible inlet irrotational isentropic flow linearized Mach number Mach waves mass flow rate molecular molecules momentum equation normal shock normal shock wave oblique shock obtain occur one-dimensional flow perfect gas piston plug nozzle Prandtl Meyer pressure and temperature pressure ratio problem psia Rayleigh reservoir resultant shock wave shown in Figure solution stagnation pressure stagnation temperature static pressure steady flow subsonic flow supersonic flow surface test section Thermodynamics throat area tube velocity of sound versus wall wedge