مدل سازی ناپایداری های آیرودینامیکی جریان در موتورهای هوایی

[1] Farokh.i S., Aircraft Propulsion, John Wiley & Sons,Inc, 2009.

[2] Cohen H., G. Rogers, Saravanamutto H., Gas Turbine Theory, 3^rd Edittion, Longman Sciectific and Technical Publications,1987.

[3] McNulty S.G., A Study Of Dynamic Compressor Surge Control Strategies for a Gas Turbine Engine, M.S. Thesis, Department of Aeronautics and Astronautics, MIT, 1993.

[4]Fischer K. and Thoma D., Investigations of the Flow Conditions in aCentrifugal Pump, Transactions of ASME, Vol. 54, pp. 141-155, Nov. 1932.

[5]Greitzer E. M., Surge and Rotating Stall in Axial Flow Compressor: Part 1,Theoretical Compression System Model, and Part 2, Experimental Results and Comparison with Theory, ASME Journal of Engineering for Power Transactions ÷of ASME, Vol. 98, pp. 190-217, April 1976.

[6]Xingen Lu., Wuli Chu., Junqiang Zhu., Zhiting Ton, Numerical and Experimental Investigations of SteadyMicro-Tip Injection on a Subsonic Axial-Flow Compressor Rotor, Hindawi Publishing Corporation International Journal of Rotating Machinery,Volume 2006

[7]Sebghati J. M., Monitoring Axial-Flow Compressor Rotating Stall and Surge, Master’s Thesis, The University of Tennessee, Knoxville, May 1992

[8] Vishwas I., Jimmy T., Niazi S., Numerical Studies of Two Approaches for Surge Control in Axial Compressors, School of Aerospace Engineering Georgia Institute of Technology,Atlanta, 2003.

 [9] Kaplan W., Ch. 2 in Advanced Calculus, 3rd Ed., Adison-Wesley Publishing

co., 1984

[10] Niazi, S., Stein A., and Sankar L.N., Computational Analysis of Stall Control Using Bleed Valve in a High-Speed Compressor, AIAA Paper 2000-3507

[11] Ghafari A., Offer an Improved Model for Investigation of Surge And Rotating Stall in Axial Flow Compressor WithVariable Speed, Proceedings ofThe 9th Conference of Iranian Aerospace Society, Tehran, Iran, February 8-10, 2010.