بررسی عددی و رفتار شناسی جریان درون تونل های باد فرا صوت دمشی در مرحله راه اندازی

Anderson, J.D. “Gas dynamic Lasers: An Introduction”, Academic, New York, 1976.

Anderson, J.D. “Modern Compressible Flow: with Historical Perspective”, second ed., McGraw-Hill, New York, 1990.

Pope, A., Goin, K.L. “High-Speed Wind Tunnel Testing”, Wiley, New York, 1965.

Hamed, A., Shang, J.S. “Survey of validation data base for shockwave boundary-layer interactions in supersonic inlets”, J. Propulsion Power 7 (4) pp. 617-625, 1991.

Polsky, S.T., Cambier, J.L. “ Numerical study of transient flow phenomena in shock tunnels”, AIAA J. 32 (5) pp. 971-978, 1994.

Chen, C.L., Chakravarthy, S.R. “ Numerical investigation of separated nozzle flows”, AIAA J. 32 (9) pp. 1836-1843, 1994.

Argrow, B.M., Emanuel, G. “Computational analysis of the transonic flow field of two-dimensional minimum length nozzle”, J. Fluid Eng., Trans. ASME 113 pp. 479-488, 1991.

Causon, D.M., Ingram, D.M., Yang, G. “On applications of high resolution shock capturing methods to unsteady flows”, in:E.F. Toro,J. F. Clarke (Eds.), Numerical Methods for Wave Propagation, Fluid Mechanics and its Applications, vol. 47, Kluwer Academic Publishers. Dordrecht. Pp. 145-171, 1995.

Reddy, D.R., Weir, L.J. “Three-dimensional viscous analysis of a much 5 inlet and comparison with experimental data”, J. Propulsion Power 8 (2) pp. 432-440, 1992.

Hsia, Y.C., Gross, B.J., Ortwerth, J.P. . “ Inviscid analysis of a dual mode scramjet inlet”, J. Propulsion Power 7 (6) pp. 1030-1035, 1991.

Hsia, Y.C., Daso, E.w., Padhye, V.A. “Full Navier-Stokes analysis of a three-dimentional scramjet inlet”, J. Propulsion Power 8 (5) pp. 1071-1078, 1992.

Hsia, Y.C. “Full Navier-Stokes analysis of an axisymmetric scramjet inlet”, J. Propulsion power 9 (6) pp. 827-833, 1993.

Korte, J.J., Singh, D.J., Auslender, A.A. “ Numerical study of the performance of swept, curved, compression surface scramjet inlets”, J. Propulsion power 10 (6) pp. 841-847, 1994.

Spalart, PR., Allmaras, SR. “A one-equation turbulent model for aerodynamic flows”. AIAA Paper 92-0439, 1992.

Joa˜o B.P. Falca˜o Filho, Marcos A. Ortega. “Numerical study of the injection process in a transonic wind tunnel: The numerical details”, Computers & Fluids 37 pp. 1276–1308, 2008.

Joa˜o B.P. Falca˜o Filho, Marcos A. Ortega, Numerical study of the injection process in a transonic wind tunnel. Part II: The off-design points, Computers & Fluids 38 pp. 888–898, 2009.