[1] Nili Ahmadabadi M, Ghadak F, Mohammadi M (2014) Quasi-Three-dimensional aerodynamic design of S-shaped air intake using inverse design method. Journal of Modares Mechanical Engineering 14(4): 189-199. (In persian)

[2] Papadopoulos F, Valakos I, Nikolos IK (2012) Design of an S‐duct intake for UAV applications. Aircr Eng Aerosp Tec 84(6): 439-456.

[3] Benini E, Furlan F, Savill M, Chiereghin N, Kipouros T (2014) Computational design of S-Duct intakes for distributed propulsion. Aircr Eng Aerosp Tec 86(6): 473-477.

[4] Lee J, Cho J (2018) Effect of aspect ratio of elliptical inlet shape on performance of subsonic diffusing S-duct. J Mech Sci Technol 32(3): 1153-1160.

[5] Yurko I, Bondarenko G (2014) A new approach to designing the S-shaped annular duct for industrial centrifugal compressor. Int J Rotating Mach 2014: 10.

[6] Jirasek A (2006) Design of vortex generator flow control in inlets. J Aircraft 43(6): 1886-1892.

[7] Tanguy G, MacManus DG, Zachos P, Gil-Prieto D, Garnier E (2017) Passive flow control study in an S-duct using stereo particle image velocimetry. AIAA J 55(6): 1862-1877.

[8] Hamstra JW, Miller DN, Truax PP, Anderson BA, Wendt BJ (2000) Active inlet flow control technology demonstration. Aeronaut J 104(1040): 473-479.

[9] Da X, Fan Z, Fan J, Zeng L, Rui W, Zhou R (2015) Microjet flow control in an ultra-compact serpentine inlet. Chinese J Aeronaut 28(5): 1381-1390.

[10] Ziaei-Rad S, Ziaei-Rad M (2006) Inverse       design of supersonic diffuser with flexible walls using a Genetic Algorithm. J Fluid Struct 22(4): 529-540.

[11] Amitay M, Pitt D, Glezer A (2002) Separation control in duct flows. J Aircraft 39(4): 616-620.

[12] Bandar Saheby E, Olyaei G, Kebriaee A (2017) Design and numerical analysis of Mach 3.0 inlet. Journal of  Modares Mechanical Engineering 17(4): 199-208. (In Persian)

[13] Bondar Saheby E, Olyaei G, Kebriaee A, Huang G (2017) Effect of thick boundary layer ingestion on the performance of hypersonic inlet. Journal of Modares Mechanical Engineering 17(10): 73-80. (In Persian)

[14] Nili Ahmadabadi M, Ghadak F, Mohammadi M, Nejati A (2012) 2-D aerodynamic design of turbojet engine S-shaped air intake considering the engine nose effects. Journal of Solid and Fluid Mechanics 1(1): 59-69. (In Persian)

[15] Gerolymos GA, Joly S, Mallet M, Vallet I (2010) Reynolds-stress model flow prediction in aircraft-engine intake double-S-shaped duct. J Aircraft 47(4): 1368-1381.

[16] Gerolymos GA, Vallet I (2016) Reynolds-stress model prediction of 3-D duct flows. Flow Turbul Combust 96(1): 45-93.

[17] Taskinoglu ES, Knight DD (2004) Multi-objective shape optimization study for a subsonic submerged inlet. J Propul Power 20(4): 620-633.

[18] D’Ambros A, Kipouros T, Zachos P, Savill M, Benini E (2018) Computational design optimization for S-ducts. Designs 2(4): 36.

[19] Othmer C (2014) Adjoint methods for car aerodynamics. J Math Ind 4(1): 6.

[20] Azimi A, Goudarzi P, Gholami S (2014) Contact boundary condition estimation in fractional non-fourier heat conduction problem using conjugate gradient method without/with adjoint problem. Journal of Modares Mechanical Engineering 14(6): 22-28. (In Persian)

[21] Tonomura O, Kano M, Hasebe S (2010) Shape optimization of microchannels using CFD and adjoint method. Comput-Aided Chem En 28: 37-42.

[22] Jin W, Taghavi R (2008) A computational study of icing effects on performance of S-duct inlets. AIAA J.

[23] Mohler S (2004) Wind-us flow calculations for the M2129 S-duct using structured and unstructured grids. AIAA J.

[24] Garshasbi M, Jafari MM, Parhizkar H (2019) Numerical analysis of flow separation control on a BWB drone using a vortex generator. Journal Of Modares Mechanical Engineering 19(2): 447-456. (In Persian)

[25] Seddon J, Goldsmith EL (1999) Intake aerodynamic. Blackwell Science.