[1] Simmons FS (2000) Rocket exhaust plume phenomenology. The Aerospace Press, USA.
[2] Dennis C, Sutton P (2005) Assessing rocket plume damage to launch vehicles. 41st AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Arizona, USA, AIAA 2005-4163.
[3] Niu Q, Duan X, Meng X, He Z, Dong S (2019) Numerical analysis of point-source infrared radiation phenomena of rocket exhaust plumes at low and middle altitudes. Infrared Phys Technol 99: 28–38.
[4] Watts D (2016) Assessing computational fluid dynamics turbulence models for rocket exhaust plume simulation. 52nd AIAA/SAE/ASEE Joint Propulsion Conference, USA, 4591.
[5] Dennis CW (1996) A study of rocket exhaust particles. PhD Thesis, Cranfield University, UK.
[6] Cousins JM (1982) Calculations of conditions in an axisymmetric rocket exhaust plume: The REP3 computer program. RARDE, Westcott, UK.
[7] Pu P, Jiang Y (2019) Assessing turbulence models on the simulation of launch vehicle base heating. Int J Aerosp Eng 1: 4240980.
[8] Fontes DH, Metzger PT (2022) Evaluation of different RANS turbulence models for rocket plume on Mars environment. AIAA SCITECH 2022 Forum, USA, 0741.
[9] Childs RE, Matsuno KV (2024) Novel turbulence model tailored for complex rocket motor exhaust jets. AIAA AVIATION Forum and Exposition.
[10] Sanford G, McBride B (1996) Computer program for calculation of complex chemical equilibrium compositions and applications. NASA Reference Publication.
[11] Langenais A, Aubrée J, Doublet P, Langlois S, Rialland V (2023) Numerical simulation of flight effect on the afterburning plume exhausting from a solid rocket motor. EUCASS-CEAS 2023, Switzerland.
[12] Chase MW (1985) NIST-JANAF thermochemical tables. J Phys Chem Ref Data.
[13] Spalart PR, Allmaras SR (1994) A one-equation turbulence model for aerodynamic flows. Rech Aerospatiale 1: 5–21.
[14] Launder BE, Spalding DB (1974) The numerical computation of turbulent flows. Comput Methods Appl Mech Eng 3(2): 269–289.
[15] Bardina JE, Huang PG, Coakley TJ (1997) Turbulence modeling validation, testing, and development. NASA Technical Memorandum 110446.
[16] Shih TH, Liou WW, Shabbir A, Yang Z, Zhu J (1995) A new k-ε eddy viscosity model for high Reynolds number turbulent flows—Model development and validation. Comput Fluids 24(3): 227–238.
[17] Orszag SA, Yakhot V, Flannery WS, Boysan F, Choudhury D, Maruzewski J, Patel B (1993) Renormalization group modeling and turbulence simulations. International Conference on Near-Wall Turbulent Flows, Arizona, USA.
[18] Wilcox DC (1998) Turbulence modeling for CFD. DCW Industries, Canada.
[19] Zhou X, Luo KH, Williams J (2001) Large-eddy simulation of a turbulent forced plume. European J. Mech. - B/Fluids 20(2):233-254.
[20] Thies A, Tam CKW (1996) Computation of turbulent axisymmetric and non-axisymmetric jet flows using the k-ε model. AIAA J 34(2): 309–316.
[21] Roblin A, Dubois I, Grisch F, Boischot A, Vingert L (2002) Comparison between computations and measurements of a H2/LOX rocket motor plume. 8th AIAA/ASME Joint Thermophysics and Heat Transfer Conference, Missouri, USA, AIAA-2002-3107.
[22] Chien KY (1982) Predictions of channel and boundary-layer flows with a low-Reynolds number turbulence model. AIAA J 20(1): 33–38.
[23] Kato M, Launder BE (1993) The modeling of turbulent flow around stationary and vibrating square cylinders. Proc 9th Symposium on Turbulent Shear Flows, Kyoto, Japan, 10.4.1–10.4.6.
[24] Friedrich R (2004) Fundamentals of compressible turbulence. IV Escloa de Primavera de Transicao e Turbulencia.
[25] Menter FR (1993) Zonal two equation k-ω turbulence models for aerodynamic flows. 24th AIAA Fluid Dynamics Conference, Orlando, USA, AIAA-93-2906.
)