Aerodynamic Performance Prediction Model for Microscale Supersonic Axial Compressor
Author:
Affiliation:
1. College of Science and Engineering, Ritsumeikan University
Publisher
Institute of Electrical Engineers of Japan (IEE Japan)
Link
https://www.jstage.jst.go.jp/article/ieejsmas/144/8/144_206/_pdf
Reference44 articles.
1. (1) A. Epstein : “Millimeter-Scale, Micro-Electro-Mechanical Systems Gas Turbine Engines”, Journal of Engineering for Gas Turbines and Power, Vol. 126, No. 2, pp. 205-226 (2004)
2. (2) R. Deam, E. Lemma, B. Mace, and R. Collins : “On Scaling Down Turbines to Millimeter Size”, Journal of Engineering for Gas Turbines and Power, Vol. 130, No. 5, pp. 052301-1-052301-9 (2008)
3. (3) B. Sirakov, Y. Gong, A. Epstein, and C. Tan : “DESIGN AND CHARACTERIZATION OF MICROCOMPRESSOR IMPELLERS”, ASME Turbo Expo 2004, Vol. 5, No. GT2004-53332, pp. 737-746 (2004)
4. (4) Y. Gong, B. Sirakov, A. Epstein, and C. Tan : “AEROTHERMODYNAMICS OF MICROTURBOMACHINERY”, ASME Turbo Expo 2004, Vol. 6, No. GT2004-53877, pp. 95-102 (2004)
5. (5) S. Tanaka, T. Nakai, and T, Toriyama : “Analysis of aerodynamic performance of high-speed rotational components for MEMS based turbomachinery considering effects of tip clearance and diabatic heat transfer”, IEEJ Trans. SM, Vol. 141, No. 6, pp. 164-172 (2021)
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