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Handbook of Turbomachinery Second Edition Revised - Ventech!

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4. Better instrumentation for heat-transfer and aerodynamic studies.<br />

There is a great need for nonintrusive wide-area sensing devices, particularly<br />

for temperature and pressure that can be read at high rates. The sensors or<br />

sensing media will most likely need to be read optically to give a 2D surface<br />

field <strong>of</strong> information at one time. This would solve a number <strong>of</strong> difficult<br />

problems encountered using today’s technology. In particular, limitations<br />

on sensor placement and wire routing and breaking would be eliminated.<br />

Acknowldgements<br />

The author wishes to thank Dr. Richard Rivir, Mr. Jeffrey Stricker, and Ms.<br />

Renee Kaffenbarger <strong>of</strong> the Air Force Research Laboratory, Pr<strong>of</strong>. Michael<br />

Dunn <strong>of</strong> Ohio State University, and Pr<strong>of</strong> Michael Crawford <strong>of</strong> University <strong>of</strong><br />

Texas. Thanks, too, to Dr. Louis Povinelli, Dr. Raymond Gaugler, and Mr.<br />

Robert Boyle <strong>of</strong> NASA/Glenn Research Center, and to Dr. David Wistler<br />

<strong>of</strong> the General Electric Company for their kind assistance. Ms. Dayna<br />

Groeber <strong>of</strong> RCF Information Systems Inc. did outstanding work in<br />

preparing the illustrations. Finally, I’d like to thank my loving wife, Joanne,<br />

for her contribution.<br />

REFERENCES<br />

1. J. H. Horlock, Axial Flow Turbines Fluid Mechanics and Thermodynamics,<br />

Butterworth and Co. Ltd., London, 1966.<br />

2. C. H. Wu, ‘‘A Generalized Theory <strong>of</strong> Three-Dimensional Flow in Subsonic and<br />

Supersonic Turbomachines <strong>of</strong> Axial, Radial, and Mixed Flow Types,’’ NACA<br />

Tech. Note 2604 (1952).<br />

3. T. Katsanis and McNally, ‘‘FORTRAN Program for Calculating Velocities<br />

and Streamlines on the Hub-Shroud Mid-Channel Stream Surface <strong>of</strong> an Axial-,<br />

Radial-, or Mixed Flow Turbomachine or Annular, Duct, Vol. 1 User’s<br />

Manual, Vol. 11 Programmer’s Manual,’’ NASA TND-8430, 8431 (1977). See<br />

also: R. A. Novak and Hearsay, ‘‘A Nearly Three Dimensional Intrablade<br />

Computing System for <strong>Turbomachinery</strong>,’’ ASME-76-FE-19 and -20, 1976.<br />

4. T. Katsanis ‘‘FORTRAN Program for Calculating Transonic Velocities on a<br />

Blade-to-Blade Stream Surface <strong>of</strong> a Turbomachine,’’ NASA TN D5427 (1969).<br />

5. S. V. Patankar and D. B. Spalding, Heat and Mass Transfer in Boundary<br />

Layers, Morgan-Grampian Press, London, 1967.<br />

6. D. A. Anderson, J. C. Tannehill, and R. H. Pletcher, Computational Fluid<br />

Mechanics and Heat Transfer, Hemisphere Publishing Co., New York, 1984.<br />

7. M. E. Crawford, ‘‘Simulation Codes for Calculation <strong>of</strong> Heat Transfer to<br />

Convectively Cooled Turbine Blades,’’ in Convective Heat Transfer and Film<br />

Copyright © 2003 Marcel Dekker, Inc.

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