A platform for research: civil engineering, architecture and urbanism
Influence of nozzle exit tip thickness on the performance and flow field of jet pump
JOURNAL OF MECHANICAL SCIENCE AND TECHNOLOGY ; 22 ; 1959-1965
2008-01-01
7 pages
Article (Journal)
English
DDC:
621
© Metadata Copyright the British Library Board and other contributors. All rights reserved.
INFLUENCE OF NOZZLE EXIT CROSS SECTION SHAPE ON PERFORMANCE OF JET PUMP
British Library Conference Proceedings | 2007
|British Library Online Contents | 2017
|Numerically analyzed supersonic flow structure behind the exit of a two-dimensional micro nozzle
British Library Online Contents | 2008
|Manufacturing method of the exit cone for propulsion nozzle unit
European Patent Office | 2015