Zobrazeno 1 - 10
of 35
pro vyhledávání: '"Schlieren photograph"'
Publikováno v:
The Journal of Engineering (2019)
Gas-to-liquid (GTL) transformer oil is increasingly considered as an alternative to conventional mineral oils, due to its consistent performance, high purity and essentially free of sulphur. This high interest has led to growing research attention on
Externí odkaz:
https://doaj.org/article/98955566458a4542b2690f2cc38cbe33
Publikováno v:
The Journal of Engineering (2019)
Gas-to-liquid (GTL) transformer oil is increasingly considered as an alternative to conventional mineral oils, due to its consistent performance, high purity and essentially free of sulphur. This high interest has led to growing research attention on
Externí odkaz:
https://explore.openaire.eu/search/publication?articleId=doi_dedup___::f92f4ef849bab10caa763bfab2e7490c
https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8366
https://digital-library.theiet.org/content/journals/10.1049/joe.2018.8366
Publikováno v:
宇宙輸送シンポジウム 平成15年度 = Proceedings of Space Transportation Symposium FY2003. :135-138
資料番号: AA0047118034
Publikováno v:
宇宙輸送シンポジウム 平成15年度 = Proceedings of Space Transportation Symposium FY2003. :139-142
In the present study were examined numerically and experimentally the off-design performance characteristics on an axisymmetric plug nozzle with variable throat area. In this nozzle concept its throat area can be changed by translating the plug in th
Publikováno v:
日本機械学会論文集. B編. 69(683):1570-1576
This paper describes an experimental study on the internal structure of the Mach 4 pseudo-shock wave (PSW) in a straight square duct with cross section of 80×80 mm^2, using the new Mach 4 supersonic wind tunnel of Muroran Institute of Technology. Th
Publikováno v:
TRANSACTIONS OF THE JAPAN SOCIETY OF MECHANICAL ENGINEERS Series B. 68:3295-3301
In order to investigate the supersonic flow phenomena related to internal and external flows of high-pressure gas pipeline systems, new air breathing engines and space planes, a new supersonic wind tunnel (pressure-vacuum type, Mach 2.0 and 4.0) was
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 45:29-39
20-21 May 1999 (62nd). 25-26 Nov. 1999 (63rd)
航技研超音速風洞の測定部断面(1m×1m)の圧力を15本のピトー管(総圧管)からなる櫛型プローブ、および高速多点圧力計測装置(ZOCシステム)を用いて計
航技研超音速風洞の測定部断面(1m×1m)の圧力を15本のピトー管(総圧管)からなる櫛型プローブ、および高速多点圧力計測装置(ZOCシステム)を用いて計
Autor:
Ishii, Ryuji, Yui, Masatoshi
Publikováno v:
航空宇宙技術研究所特別資料 = Special Publication of National Aerospace Laboratory. 37:289-293
航空宇宙技術研究所 12-13 Jun. 1997 東京 日本
National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan
オイラー方程式に対するTVD(全変動減少)有限差分法を用いて、非定常超音速円形ジェットの
National Aerospace Laboratory 12-13 Jun. 1997 Tokyo Japan
オイラー方程式に対するTVD(全変動減少)有限差分法を用いて、非定常超音速円形ジェットの
Autor:
Job Kurian, Ramesh Kumar
Publikováno v:
Experiments in Fluids. 19:95-102
The freejet characteristics of radially lobed nozzles were studied experimentally. Schlieren photographs of the freejets revealed that the lobes of the nozzles gave rise to alternate expansion-compression regions. For two of the lobed nozzles the pot
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