[1] Fang J (1984) Application of combustion time lag theory to combustion stability analysis of liquid and gaseous propellant rocket engines. AIAA Paper.

[2]  Crocco L, Cheng SI (1956) Theory of combustion instability in liquid propellant rocket motors. Butterworths Publications Ltd, London.

[3] Wenzel LM, Szuch J (1965) Analysis of chugging in liquid-bipropellant rocket engines using propellants with different vaporizations rates. NASA TN D-3080.

[4]  Heidmann MF, Sokolowski DE, Diehl LA (1967) Study of chugging instability with liquid-oxygen and gaseous- hydrogen combustors. NASA TND-4005.

[5]  Wood DJ, Dorsch R (1967) Effect of propellant feed system coupling and hydraulic parameters on analysis of chugging. NASA TN D-3896.

[6] Kahn DR (1975) Orbital maneuvering engine-feed system coupled stability investigation. NASA CR-150944.

[7]  Lim KC, George PE (1987) Combustion stability analysis of preburners durng engine shutdown. AIAA Paper.

[8]  Ordonneau G (2000) Analysis and modeling of VULCAIN engine shutdown transient chugging. ONERA TP.

[9] Abramzon B, Sirignano WA (1989) Droplet vaporization model for spray combustion calculations. Int J Heat Mass Trans 32(9): 1605-1618.

[10] Bertoli C, Migliaccio M (1999) A finite conductivity model for diesel spray evaporation and computations, Int J Heat Fluid Flow 20: 552-561.

[11] Renksizbulut M, Yuen MC (1983) Experimental study of droplet evaporation in a high temperature air stream. ASME J Heat Transfer 105: 384-388.

[12] Zeng Y, Lee CF (2002) A preferential vaporization model for multicomponent droplets and sprays. Atomization Sprays.

[13] Wakil MM, Uyehara OA, Myers PS (1954) A theoretical investigation of the heating-up period of injected fuel droplets vaporizing in air. NACA Technical Note 3179.

[14] Reitz RD (1987) Modelling atomisation process in high-pressure vaporizing spray, atomisation and spray technology 3: 309-337.

[15] Harrje DT, Reardon FH (1972) Liquid propellant rocket combustion instability. NASA, NASA SP-194, Washington, DC.

[16] Ogata K (2002) Modern control engineering. 4th edn. Prentice-Hall, Inc., Upper Saddle River, NJ.

[17] Natanzon MS (1999) Combustion instability. Progress in Astronautics and Aeronautics, AIAA 222, Reston, VA.

[18] Bellen A,  Zennaro M, Golub GH, Schwab C, Light WA, Süli E (2003) Numerical methods for delay differential equations. Clarendon Press, Oxford.

[19] Lefebvre  AH (1989) Atomization and sprays. Hemisphere, Washington, DC.

[20] Sirignano WA (1999) Fluid dynamics and transport of droplets and sprays. Cambridge, Cambridge University Press.

[21] Dombrovsky LA, Sazhin SS, Sazhina EM, Feng G, Heikal MR, Bardsley MEA, Mikhalovsky SV (2001) Heating and evaporation of semi-transparent diesel fuel droplets in the presence of thermal radiation. Fuel 80(11): 1535-1544.

[22] Sazhin SS, Abdelghaffar WA, Sazhina EM, Mikhalovsky SV, Meikle ST, Bai C (2004) Radiative heating of semi-transparent diesel fuel droplets. ASME J Heat Trans 126: 105-109.

[23] "MATLAB®," The Mathworks, Inc., 1984-2009.

[24] Yaws CL (1999) Chemical properties handbook. McGraw-Hill, New York.

[25] Yin C (2015) Modelling of heating and evaporation of n-Heptane droplets: Towards a generic model for fuel droplet/particle conversion. Department of Energy Technology, Aalborg University, 9220 Aalborg East, Denmark, ScienceDirect 64-73.

[26] Ramezani AR (2013) Determine the range of  stability of low frequency, combustion chamber of liquid rocket engines  in terms of performance of thrust change. Iranian Combustion Institute 6(2). (In Persian)