A Course in Continuum Mechanics: Fluids, gases and the generation of thrust |
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Contents
cavitation in practice | 33 |
mentary theory of Laval nozzle | 43 |
Potential motion | 155 |
Copyright | |
3 other sections not shown
Common terms and phrases
acting applications assume basic basis body boundary layer centre chamber characteristics coefficient components compressible consequently Consider consideration constant continuous coordinate corresponding density depend derivative determined diffuser direction distribution disturbances ejector energy engines equal equation example external fact finds finite fixed flow follows forces formula function given grad heat ideal ideal fluid incompressible fluid increase infinity inside integral internal known lift force limit linked liquid mass mean mechanical medium mixing motion moving nozzle obtains Obviously particles particular plane potential presence pressure problem properties quantity radius readily region relations resistance respect resultant rigid body rotation shown side solution space sphere stagnation steady stream line supersonic surface temperature theory tion transport tube turbine turbulent vanishes vector viscous volume vortex vortices wall wave whence