Practical Use of Three-Dimensional Inverse Method for Compressor Blade Design
Author:
Affiliation:
1. Department of Mechanical, Aerospace, and Manufacturing Engineering Syracuse University, Syracuse, NY 13244
2. Solar Turbines, Inc., San Diego, CA 92186
Abstract
Publisher
ASME International
Subject
Mechanical Engineering
Link
http://asmedigitalcollection.asme.org/turbomachinery/article-pdf/121/2/321/5840852/321_1.pdf
Reference15 articles.
1. Adamczyk J. J. , CelestinaM. L., BeachT. A., and BarnettM., 1990, “Simulation of Three-Dimensional Viscous Flow Within a Multistage Turbine,” ASME JOURNAL OF TURBOMACHINERY, Vol. 112, pp. 370–376.
2. Damle, S. V., 1998, “Fully Three-Dimensional and Viscous Inverse Method for Turbomachine Blade Design,” Ph. D. dissertation, Department of Mechanical Engineering, Syracuse University.
3. Dang, T. Q., 1995, “Inverse Method for Turbomachine Blades Using Shock-Capturing Techniques,” AIAA Paper No. 95-2465.
4. Dang, T., and Isgro, V., 1995, “Euler-Based Inverse Method for Turbomachine Blades: Part I—Two Dimensional Cascades,” AIAA Journal, Vol. 33, No. 12.
5. Dang, T., Damle, S., and Qiu, X., 1997a, “Euler-Based Inverse Method for Turbomachine Blades: Part II—Three Dimensional Flows,” submitted to AIAA Journal.
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