1. Allan, B.G., Owens, L.R., 2006. Numerical modeling of flow control in a boundary-layer-ingesting offset inlet diffuser at transonic mach numbers. In: Proc. of 44th AIAA Aeropace Sciences Meeting and Exhibit, Nevada, Reno (Print).
2. Separation control in duct flows;Amitay;J. Aircraft,2002
3. Anabtawi, A.J., Blackwelder, R.F., Lissaman, P.B.S., Liebeck, R.H., 1999. An experimental investigation of boundary layer ingestion in a diffusing S-duct with and without passive flow control. In: Proc. of 37th AIAA Aerospace Sciences Meeting and Exhibit, Nevada, Reno (Print).
4. Anderson, B.H., Levy, R., 1991. Vortex generator design for aircraft inlet distortion as a numerical optimization problem. In: Proc. of 3rd International Conference on Inverse Design Concepts and Optimization in Engineering Sciences, Washington, D.C. Ed. G. S. Dulikravich, pp. 419–432 (Print).
5. Anderson, B.H., D.N. Miller, Addington, G.A., Agrell, J., 2004. “Optimal Micro-Vane Flow Control for Compact Air Vehicle Inlets” NASA/TM-2004-0212936 (Print).