Cryogenic Wind Tunnel

In order to get high Reynolds number flows in a wind tunnel, it is the best way to use a gas of small kinematic viscosity by making temperature lower and pressure higher in the closed wind tunnel. About 20 of cryogenic wind tunnels are being used in the world. In this report, at first, its principle...

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Published inJournal of Japan Society of Fluid Mechanics Vol. 11; no. 1; pp. 14 - 23
Main Author ADACHI, Tsutomu
Format Journal Article
LanguageJapanese
Published The Japan Society of Fluid Mechanics 1992
Subjects
Cryogenic wind tunnel
High Reynolds number flow
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Abstract In order to get high Reynolds number flows in a wind tunnel, it is the best way to use a gas of small kinematic viscosity by making temperature lower and pressure higher in the closed wind tunnel. About 20 of cryogenic wind tunnels are being used in the world. In this report, at first, its principle, structure and characteristics are described. Then a look of several representative ones in the world are given. The status of researches using cryogenic wind tunnels are also described.
AbstractList In order to get high Reynolds number flows in a wind tunnel, it is the best way to use a gas of small kinematic viscosity by making temperature lower and pressure higher in the closed wind tunnel. About 20 of cryogenic wind tunnels are being used in the world. In this report, at first, its principle, structure and characteristics are described. Then a look of several representative ones in the world are given. The status of researches using cryogenic wind tunnels are also described.
Author ADACHI, Tsutomu
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References 3) CRYO Newsletter, No.4, June, (NASA 1990).
8) X. Bouis, The European Transonic Windtunnel (ETW), AGARD-Report-774 (1989), 6-1-16.
13) M. C. Lewis, Aerofoil Testing in a Self-Streaming Flexible Walled Wind Tunnel, NASA Contractor Report 4128 (1988), 1-257.
5) S. Balakrishna and W. A. kilgore, Microcomputer Based Controller for the Langley 0.3-Meter Transonic Cryogenic Tunnel, NASA Controller Report 181808 (March-1989), 1-147.
9) A. Seraudie, J-P. Archambaud, A. Blanchard and J-B. Dor, T2 Cryogenic Transonic Wind Tunnel Thermal Design and Control of the Facility Including Models Adapted for Short Run Processing, ASME / JSME Thermal Engineering Proceedings Vol. 5 (1991-3), 379-386.
10) A. M. Clausing, Advantages of a Cryogenic Environment for Experimental Investigations of Convective Heat Transfer, Int. J. Heat Mass Transfer, 25-8 (1982), 1255-1257.
12) H. Försching, E. Melzer and G. Schewe, Ein neuer Windkanal für gebäudeaerodynamische und-aeroelastische Untersuchungen bei Reynoldszahlen bis 107, Konstruktiver Ingenieurbau Berichte, Heft 35/36, 1981,127-133.
6) A. L. Iskra, N. K. Mikhailov, A. P. Philatov and V. P. Rukavets, TsAGI Cryogenic Transonic Wind Tunnel T-134, ASME/JSME Thermal Engineering Proceedings Vol. 5 (1991-3), 387-391.
2) T. Adachi, K. Matsuuchi and T. Kawai, High Reynolds Number Flow Experiments using Cryogenic Wind Tunnel, ASME/JSME Thermal Engineering Proceedings, Vol. 5 (1991-3), 371-378.
11) G. Hefer, The Cryogenic Ludwig Tube Tunnel At Göttingen, AGARD Report-774 (1989), 8-1-7.
4) J. F. Campbell, The National Transonic Facility-A Research Perspective, AIAA-84-2150 (1984), 1-7.
14) 安達勤, 小野博基, 松内一雄, 河合達雄, 長哲夫, 高レイノルズ数領域における円柱まわりの流れ (表面粗さの影響), 日本機械学会論文集 (B編) 55-511 (1989-3), 685-691.
1) P. L. Lawing, R. L. Kilgore and P. D. McGuire, Cryogenic Wind Tunnels for High Reynolds Number Testing, NASA T. M. 87743 (1986-5), 1-89.
7) A. I. Omelaev and A. M. Kharitonov, A Cooling System In Transonic Cryogenic Wind Tunnel Being Under Construction At Institute Of Theoretical And Applied Mechanics, ASME/JSME Thermal Engineering Proceedings Vol. 5 (1991-3), 409-413.
15) 安達勤, 小野博基, 松内一雄, 河合達雄, 長哲夫, 高レイノルズ数領域における円柱の抵抗と発生うず例 (表面粗さの影響), 日本機械学会論文集 (B編) 55-517 (1989-9), 2597-2601.
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High Reynolds number flow
Title Cryogenic Wind Tunnel
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