Analysis of Aerodynamic Components Matching for Microscale Gas Turbine Engine
Author:
Affiliation:
1. College of Science snd Engineering, Ritsumeikan University
Publisher
Institute of Electrical Engineers of Japan (IEE Japan)
Subject
Electrical and Electronic Engineering,Mechanical Engineering
Link
https://www.jstage.jst.go.jp/article/ieejsmas/138/4/138_132/_pdf
Reference15 articles.
1. (1) T. J. Mueller : “FIXED AND FLAPPING WING AERODYNAMICS FOR MICRO AIR VEHICLE APPLICATIONS”, AIAA (2010)
2. (2) M. Namura and T. Toriyama : “Aero-Thermodynamic Consideration of Single-Crystal-Silicon Premixed-Fuel Microscale Can Combustor”, Journal of Engineering for Gas Turbines and Power, Vol. 134, No. 7, pp. 071501-1-071501-11 (2012)
3. (3) M. Namura and T. Toriyama : “Experimental Study on Aerodynamics of Microelectromechanical Systems Based Single-Crystal-Silicon Microscale Supersonic Nozzle”, Journal of Fluids Engineering, Vol. 135, No. 8, 081101-1-081101-11 (2013)
4. (4) A. H. Epstein : “Millimeter-Scale, Micro-Electro-Mechanical System GAS TURBINE ENGINES”, Journal of Engineering for Gas Turbines and Power, Vol. 126, pp. 205-226 (2004)
5. (5) R. T. 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)
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