Automatic Optimization of Preswirl Nozzle Design
Author:
Affiliation:
1. Fluids Research Centre, School of Engineering, University of Surrey, Guildford, Surrey GU2 7XH, UK
2. Rolls-Royce plc, PO Box 31, Derby DE24 8BJ, UK
Abstract
Publisher
ASME International
Subject
Mechanical Engineering,Energy Engineering and Power Technology,Aerospace Engineering,Fuel Technology,Nuclear Energy and Engineering
Link
http://asmedigitalcollection.asme.org/gasturbinespower/article-pdf/129/2/387/5587727/387_1.pdf
Reference13 articles.
1. Meierhofer, B., and Franklin, C. J., 1981, “An Investigation of Preswirled Cooling Airflow to a Turbine Disc by Measuring the Air Temperature in the Rotating Channels,” ASME Paper No. 81-GT-132.
2. Dittman, M., Geis, T., Schramm, V., Kim, S., and Wittig, S., 2001, “Discharge Coefficients of a Pre-Swirl System in Secondary Air Systems,” ASME Paper No. 2001-GT-0122.
3. Geis, T., Dittmann, M., and Dullenkopf, K., 2003, “Cooling Air Temperature Reduction in a Direct Transfer Preswirl System,” ASME Paper No. GT2003-38231.
4. Wilson, M., Pilbrow, R., and Owen, J. M., 1995, “Flow and Heat Transfer in a Pre-Swirl Rotor-Stator System,” ASME Paper No. 95-GT-239.
5. Chew, J. W., Hills, N. J., Khalatov, S., Scanlon, T., and Turner, A. B., 2003, “Measurement and Analysis of Flow in a Pre-Swirled Cooling Air Delivery System,” ASME Paper No. GT2003-38084.
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