A Novel Three-Dimensional Inverse Method for Axial Compressor Blade Surface Design
Author:
Funder
National Natural Science Foundation of China
Publisher
Springer Science and Business Media LLC
Subject
Multidisciplinary
Link
http://link.springer.com/content/pdf/10.1007/s13369-019-04083-3.pdf
Reference31 articles.
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2. Sanz, J.M.: Lewis Inverse Design Code (LINDES): Users Manual. NASA Lewis Reasearch Centre, Cleveland (1987)
3. Dang, T.: A fully three-dimensional inverse method fo turbomachinery blading in transonic flows. J. Turbomach. 115(2), 354–361 (1993)
4. Dang, T.: Inverse method for turbomachine blades using shock-capturing techniques. In: 31st Joint Propulsion Conference and Exhibit, San Diego, CA (1995)
5. Dang, T.; Van, M.P.C.; Larosiliere, L.M.: Design of aspirated compressor blades using three-dimensional inverse method. In: Proceedings of ASME Turbo Expo2003, Atlanta, Georgia (2003)
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