[1] C. Warren, An experimental investigation of the effect of ejecting a coolant gas at the nose of a bluff body, Fluid Mechanics, Vol. 8, No. 3, pp. 400-417, 1960.
[2] P. Finley, The flow of a jet from a body opposing a supersonic freestream, Fluid Mechanics, Vol. 26, No. 2, pp. 337-368, 1966.
[3] V. Fomin, A. Maslov, A. Shashkin, Flow regimes formed by a counterflow jet in a supersonic flow., Fluid Mechanics, Vol. 42, No. 5, pp. 757-764, 2001.
[4] K. Hayashi, S. Aso, Y. Tani, Numerical study of thermal protection system by opposing jet, 43th AIAA Aerospace Sciences Meeting, Reno, Nevada, Jan. 10-13, 2005.
[5] I. Tamada, S. Aso, Y. Tani, Numerical study of the effect of the opposing jet on reduction of aerodynamic heating with different nose configurations, 26th International Congress of the Aeronautical Sciences, Anchorage, AL, Sep. 14–19, 2008.
[6] I. Tamada, S. Aso, Y. Tani, Reducing aerodynamic heating by the opposing jet in supersonic and hypersonic flows, 48th AIAA Aerospace Sciences Meeting, Florida, Orlando, Jan. 4-7, 2010.
[7] L. Bin, W. Zhen, H. Wei, Effect of the injector configuration for opposing jet on the drag and heat reduction, Aeropace Science and Technology, Vol. 51, No. 1, pp. 78-86, 2016.
[8] M. Mumivand, H. Mohammadkhani, Numerical stydy of aerodynamic drag reduction of blunt nose with hybrid of spike and axial and lateral jet injection, Modares Mechanical Engineering, Vol. 16, No. 7, pp. 133-142, 2017. (in (فارسی Persian
[9] S. Abdollahi, A. Mardani, S. A. Seyed Shams Talghani, Effects of Pulsed counterflow jets on aerothermodynamics performance of a supersonic reentry capsule, Aerospace Knowledge and Technology, Vol. 5, No. 1, pp. 55-65, 2017. (in Persian فارسی(
[10] F. Menter, M. Kuntz, R. Langtry, Ten years of industrial experience with the SST turbulence model, Heat and Math Transfer, Vol. 51, No. 4, pp. 625-632, 2003.
[11] M. S. Liou, J. Steffen, A new flux splitting scheme, Computational Physics, Vol. 107, No. 3, pp. 23-39 1993.
[12] J. Blazek, Computational Fluid Dynamics: Principles and Applications, pp. 305-320, New York: Wiley, 1989.
[13] D. C. Wilcox, Turbulence Modeling for CFD, pp. 325-326, California: DCW industries, 1998.
[14] M. Tahani, M. Hojaji, M. Salehifar, A. Dartoomain, Numerical investigation of sonic jet injection effects of flow field structure and thrust vector control performance in a supersonic nozzle, Modares Mechanical Engineering, Vol. 13, No. 4, pp. 74-85, 2013. (in Persian فارسی(
[15] M. H. Shojaeefard, M. Tahani, M. Ehghaghi, Numerical study of the effects of some geometric characteristics of a centrifugal pump impeller, Computers&Fluids, Vol. 60, No. 1, pp. 61-70, 2012.
[16] M. Tahani, M. S. Karimi, A. Mahmoudi Motlagh, Numerical investigation of drag and heat reduction in hypersoinc spiked blunt bodies, Heat Mass Transfer, Vol. 49, No. 10, pp. 757-764, 2013.
[17] S. P. Anjalidevi, S. Aruna, Effect of counterflow jet on attenuation of drag and aerodynamic heating aver a coneogive body in hypersonic flow, Applied Mathematics and Mechanics, Vol. 7, No. 4, pp.95-122, 2011.
[18] J. E. Bardina, P. Huang, Turbulence modeling validation testing and development, Nasa Technical Memorandum 110446, 1997.
[19] K. Kitamura, E. Shima, Three dimentional carbuncles and euler fluxes, 48th AIAA Aerospace Sciences Meeting, Florida, Orlando, January 4-7, 2010.
[20] M. Tahani, M. Hojaji, A. Dartoomian, M. Salehifar, Numerical Analysis of attack angle effects on 3D supersonic turbulent flow around blunt body along with opposite jet injection, Modares Mechanical Engineering, Vol. 17, No. 3, pp. 355-366, 2017. (in Persian فارسی(