The Compressible Calibration of Miniature Multi-Hole Probes

Author:

Johansen Espen S.1,Rediniotis Othon K.2,Jones Greg3

Affiliation:

1. Department of Mechanical Engineering, Texas A&M University, College Station, TX 77843-3141

2. Department of Aerospace Engineering, Texas A&M University, College Station, TX 77843-3141

3. Flow Modeling and Control Branch, NASA Langley Research Center, Hampton, VA 23681-0001

Abstract

This work presents the development of a data reduction algorithm for non-nulling, multihole pressure probes in compressible, subsonic flowfields. The algorithm is able to reduce data from any 5- or 7-hole probe and generate very accurate predictions of the velocity magnitude and direction, total and static pressures, Mach and Reynolds number and fluid properties like the density and viscosity. The algorithm utilizes a database of calibration data and a local least-squares interpolation technique. It has been tested on four novel miniature 7-hole probes that have been calibrated at NASA Langley Flow Modeling and Control Branch for the entire subsonic regime. Each of the probes had a conical tip with diameter of 1.65 mm. Excellent prediction capabilities are demonstrated with maximum errors in angle prediction less than 0.6 degrees and maximum errors in velocity prediction less than 1 percent, both with 99 percent confidence.

Publisher

ASME International

Subject

Mechanical Engineering

Reference14 articles.

1. Kjelgaard, S. O., 1988, “Theoretical Derivation and Calibration Technique of a Hemispherical-Tipped, Five-Hole Probe,” NASA Technical Memorandum 4047.

2. Bryer, D. W., and Pankhurst, R. C., 1971, “Pressure-Probe Methods for Determining Wind Speed and Flow Direction,” Her Majesty’s Stationary Office/National Physics Laboratory, The Campfield Press, St. Albans.

3. Rediniotis, O. K., Hoang, N. T., and Telionis, D. P., 1993, “The Seven-Hole Probe: Its Calibration and Use,” Forum on Instructional Fluid Dynamics Experiments, 152, June, pp. 21–26.

4. Zilliac, G. G., 1989, “Calibration of Seven-Hole Probes For Use in Fluid Flows With Large Angularity,” NASA Technical Memorandum 102200, Dec.

5. Gerner, A. A., and Maurer, C. L., 1981, “Calibration of Seven-Hole Probes Suitable for High Angles in Subsonic Compressible Flows,” United States Air Force Academy-TR-81-4.

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