Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction
From MaRDI portal
Publication:1403655
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
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
This page was built for publication: Effect of gas non-ideality on the performance of Laval nozzles with an abrupt constriction