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Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction

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Publication:1403655
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DOI10.1023/A:1021392907861zbMath1161.76366OpenAlexW124309276MaRDI QIDQ1403655

A. N. Kraĭko, K. S. P'yankov, N. I. Tillyaeva, E. V. Myshenkov

Publication date: 3 September 2003

Published in: Fluid Dynamics (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1023/a:1021392907861


zbMATH Keywords

turbulenceprofilingviscous flowsLaval nozzlesdifferential models


Mathematics Subject Classification ID

Experimental work for problems pertaining to fluid mechanics (76-05)


Related Items (6)

Inviscid gas flows in nozzles with a steeply converging contour ⋮ Contouring the nozzles producing a uniform supersonic flow or a thrust maximum in the presence of a curvilinear sonic line ⋮ Stability of one-dimensional steady flows with detonation wave in a channel of variable cross-sectional area ⋮ Comparison of air-breathing engines with slow and detonation combustion ⋮ Optimal supersonic nozzles with power-law generators ⋮ Hysteresis phenomena in a plane rotatable nozzle







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