Review: Hot-Wire Anemometry in Transonic and Subsonic Slip Flows

Author:

Stainback P. C.1,Nagabushana K. A.2

Affiliation:

1. NASA Langley Research Center, Hampton, VA 23681

2. Old Dominion University Research Foundation, Norfolk, VA 23508

Abstract

In the past, only a relatively small number of investigations were conducted using hot-wire anemometry in transonic and subsonic slip flows. This was due to the complexity of the applicable equations. Now it appears that the developments in electronics and computational methods have made it practical to reconsider this problem. A review of past work performed in these flow regimes using hot-wire anemometry will be made along with a description of recent efforts made to develop methods which might be used to make measurements in these flow regimes. A detailed version of this review article is available through the electronic JFE.

Publisher

ASME International

Subject

Mechanical Engineering

Reference26 articles.

1. Barre, S., Quine, C., and Dussauge, J. P., 1992, “Compressibility Effects on the Structure of Supersonic Mixing Layers: Experimental Results,” Institute de Me´canique de Marseilles, Institut de Me´canique Statistique de la Turbulence, U.M. CNRS-Universite´ Aix-Marseille II n° 380033, 12 avenue du Ge´ne´ral Lecleerc, 13003, Marseilles, France.

2. Baldwin, L. V., 1958, “Slip-Flow Heat Transfer From Cylinders in Subsonic Airstreams,” NACA-TN-4369.

3. Demetriades, A., 1978, “Probes for Multivariant Flow Characteristics,” Proceedings of the Dynamic Flow Conference on Dynamic Measurements in Unsteady Flows, IMST, Marseille, France, pp. 13–44.

4. Hinze, J. O., 1975, Turbulence, McGraw-Hill, New York.

5. Horstman C. C. , and RoseW. C., 1977, “Hot-Wire Anemometry in Transonic Flow,” AIAA Journal, Vol. 15, No. 3, pp. 395–401.

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