[1]J.W. Hamstra, DN. Miller, PP. Truax, Active inlet flow control technology demonstration. Proceedings of the 22nd internal council of aeronautical sciences; 2000.
[2]M. B. Senseney, T. A. Buter, R. D. W. Bowersox, Performance Characterization of a Highly Offset Diffuser with Vortex Generator Jets, Journal of Propulsion and Power, Vol. 12, pp. 7,Mar-Apr, 1996.
[3] B. D. McElwain, Unsteady sparation point injection for pressure recoveryi mprovement in high subsinic diffusers. M.Sc Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, MIT, 2002.
[4] A. S. Luers, Flow control thechnics in serpentine inlet, M.Sc Thesis, Department of Aeronautics and Astronautics, Massachusetts Institute of Technology, MIT, 2003.
[5] A. C. Rabe, Effectiveness of a Serpentine Inlet Duct Flow Control Scheme at Design, PhD Thesis, Department of Mechanical Engineering, Virginia Polytechnic Institute and State University, Virginia Polytechnic Institute and State University, 2003.
[6] A. M. Pradeep, R. K. Sullerey, Secondary flow control in a circular S-duct diffuser using vortex generator jets.AIAA 2004-2615, in 2nd AIAA Flow ControlConference, Portland, Oregon, 2004.
[7] N. A. Harrison, J. Anderson, J. L. Fleming, W. F. Ng, Computational analysis of active flow control of BLI inlet.AIAA 2006-874, in 44th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2006.
[8] R. K. Sullerey, V. S. Mangat, A. Padhi, Flow control in serpentine inlet using vortex generator jets.AIAA-2006-3499, in 3rd AIAA Flow Control Conference, San Francisco, California, 2006.
[9] M. Debiasi, M. R. Herberg, Z. Yan, S. S. Dhanabalan, H. M. Tsai, Control of flow separation in S-ducts via flow injection-AIAA-2008-74, in 46th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2008.
[10] A. Gissen, B. Vukasinovic, M. McMillan, A. Glezer, Distortion management in a BLI inlet diffuser using synthetic jet hybrid flow control.AIAA2011-35-in 49th AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, 2011.
[11] N. V. Kale, Active and hybrid flow control in S-ducts and diffuser, Ph.D Thesis, Department of Aerospace Engineering, University of Illinois at Urbana-Champaign, Urbana, Illinois, 2013.
[12] A. M. Kirk, A. Kumar, J. I. Gargoloff, O. K. Rediniotis, P. G. A. Cizmas, Numerical and experimental investigation of a serpentine inlet duct, in 45th AIAA Aerospace Sciences Meeting and Exhibit, Reno, Nevada, 2007.
[13] Ansys, Ansys Fluent 15 Help, 2014.
[14] J.Shedon, Intake Aerodynamic, Second ed., UK: Blackwell Science Ltd, 1999.
[15] SAE, Inlet total pressure distortion considerations for gas turbine engines.SAE-AIR-1419A, Society of Automotive Engineers USA, pp. 2011.
[16] SAE, Gas turbine engine inlet flow distortionguidelines.SAE-ARP1420, Society of Automotive Engineers USA, pp. 2002.
[17] D. D. Sanders, M. G. List, CFD performance predictions of a serpentine diffuser configuration in an annular cascade facility.AIAA 2013-0220, in 51st AIAA Aerospace Sciences Meeting including the New Horizons Forum and Aerospace Exposition, Grapevine (Dallas/Ft. Worth Region).Texas, 2013.
[18] S. Kumar, B. Sasanapuri, K. A. Kurbatskii, A. Lestari, Pressure-based coupled simulation of pressure recovery and distortion in an S-shaped intake diffuser.AIAA 2013-3794, in 49th AIAA/ASME/SAE/ASEE Joint Propulsion Conference, San Jose, CA, 2013.
[19] T. M. Berens, A. L. Delot, M. Chevalier, J. v. Muijden, Numerical simulations for high offset intake diffuser flows.NLR-TP-2014-096, NLR, National Aerospace Laboratory NLR, pp. 2014.
[20] C. A. Nessler, W. W. Copenhaver, M. G. List, Serpentine diffuser performance with emphasis on future introduction to a transonic fan.AFRL-RQ-WP-TP-2014-0168, Vol. 1, Wright-Patterson Air Force Base, Air Force Research Laboratory, Aerospace Systems Directorate, pp. 2014.
[21] M. Rutten, S. Kuckenburgy, S. Koch, M. Rein, Investigation of the flow within partially submerged scoop type air intakes.AIAA 2013-2912, in 31st AIAA Applied Aerodynamics Conference, San Diego, CA, 2013.
[22] L. R. Owens, B. G. Allan, S. A. Gorton, Boundary-layer-ingesting inlet flow control, Journal of Aircraft, Vol. 45, No. 4, July-August, 2008.