[1] Peterson K, Hil F. Propulsion mechanics and thermodynamics; 1992 . [Book - No DOI]
[2] Cherng D, Yang V, Kuo K. Numerical study of turbulent reacting flows in solid-propellant ducted rocket combustors. Journal of Propulsion and Power. 1989; (5):678-685. DOI https://doi.org/10.2514/3.23206
[3] Stowe R. Modelling Combustor Performence of a Ducted Rocket. 36th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2000. DOI https://doi.org/10.2514/6.2000-3728
[4] Hewitt W. Numerical Modeling of a Ducted Rocket Combustor With Experimental Validation. 2008.
[5] Nakayama H, Ikegami Y, Yoshida A, Koori K, Watanabe K, Tokunaga H, Shimizu H, Kanaizumi S. Full-scale Firing Tests of Variable Flow Ducted Rocket Engines employing GAP Solid Fuel Gas Generator. 45th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit. 2009. DOI https://doi.org/10.2514/6.2009-5121
[6] Chen L, Tao C, Shan C. Study on the Side-Inlet Dump Combustor of Solid Ducted Rocket with Reacting Flow. Journal of AIAA. 1984. DOI https://doi.org/10.2514/6.1984-1378
[7] Stowe R. Performance Prediction of a Ducted Rocket Combustor. Defence Research Establishment Valcartier. 2001.
[8] Kim S, Natan B. Inlet Geomtry and Equivalence Ratio Effects on Combustion in a Ducted Rocket. Journal of Propulsion and Power. 2015;31:619-631. DOI http://dx.doi.org/10.2514/1.B35369
[9] Zhongqin Z, Zhenpeng Z, Jinfu T, Welan F. Experimental Investigation of Combustion Efficiency of air-augmented Rockets. Journal of Propuls. 1986;2(4):305-310. DOI https://doi.org/10.2514/3.22887
[10] Stowe R, Dubois C, Harris P, Mayer A, Champlain A, Ringuettes S. Two Phase Flow Combustion Modeling of a Ducted Rocket. Journal of AIAA. 2001;2001-3461. DOI https://doi.org/10.2514/6.2001-3461
[11] Zhang Y, Wu Z, Zhang Z, Chen P, Niu Y, Chen X, He Y, Fang G. Effect of Gas Injection Holes on Mixing and Combustion in Solid Propellant Ducted Rockets. Journal of Applied Thermal Engineering. vol. 2023;226. DOI https://doi.org/10.1016/2023.120212
[12] Xi W, Liu J, Mengfei R. Improvement of Mixing Efficiency in the Combustion Chamber of a Powder-Fuel Ramjet Engine. Journal of Frontiers in Energy. 2021:9. DOI https://doi.org/10.3389/fenrg.2021.756905
[13] Salva J, Tizo´n M, Jenaro G, Agudo C. Numerical Analysis of Heterogeneous Combustion in a Ducted Rocket. Journal of Aerospace Engineering. 2006;221(1):115-127. DOI http://dx.doi.org/10.1243/09544100JAERO23
[14] Wang W, Zhang G, Jun-De H. Computational Method Investigation of Solid Ducted Rocket. Journal of Engineering and Manufacturing. 2019;9(1):1-10. DOI https://doi.org/10.5815/ijem.2019.01.01
[15] Ilbas M, Karyeyen S. An experimental and numerical study on turbulent combustion of hydrogen-rich coal gases in a generated non-premixed burner. Journal of Fuel. 2017;194:274-290. DOI https://doi.org/10.1016/j.fuel.2017.01.016
[16] Karyeyen S. Combustion characteristics of a non-premixed methane flame in a generated burner under distributed combustion conditions: A numerical study. Journal of Fuel. 2018;230:163-171 . DOI https://doi.org/10.1016/j.fuel.2018.05.052
[17] Kemalettin M, Oztuna S. Numerical investigation on hydrogen-enriched methane combustion in a domestic back-pressure boiler and non-premixed burner system from flame structure and pollutants aspect. Journal of Hydrogen Energy. 2020;45(60):35246-35256. DOI https://doi.org/10.1016/j.ijhydene.2020.03.117
[18] Ansys Fluent Theory Guide 21, Ansys Inc; 2021. [Book - No DOI]
[19] Andres Z, Carvalho J, Yiguang J. Flammability Limits: A Comprehensive Review of Theory, Experiments, and Estimation Methods. Journal of Energy and Fuels. 2023;37(6):4151-4197. DOI https://doi.org/10.1021/acs.energyfuels.2c03598
[20] Ansys Fluent Users Guides 21, Ansys-Inc; 2021. [Book - No DOI]
[21] Turns S, Haworth D. An Introduction to Combustion; 2021. [Book - No DOI]
[22] McDonald B, Rice J. Solid fuel ramjet fuel optimization for maximum thrust to drag ratio and impulse density subject to geometric restraints on missle outer mold line. Journal of Aerospace Science and Technology. 2018;75:47-57. DOI https://doi.org/10.1016/j.ast.2018.01.008
[23] Jones D, Fredrick R. Ramjet Fuel Mixture Optimization. Journal of Propulsion and Energy. 2020. DOI http://dx.doi.org/10.2514/6.2020-3917
[24] Shalom A. Flammability Limits and Ballistic Propertices of Fuel-rich Propellants. Journal of Propellants, Explosives, Pyrotechnics. 1991;16(2):59-64. DOI https://doi.org/10.1002/prep.19910160204
[25] Davenas A. Development of Modern Solid Propellants. Journal of Propulsion and Power. 2003;19(6). DOI https://doi.org/10.2514/2.6947
[26] Evans V, Wiliam C, Senior R, Carson D. Experimental Characterization of a Solid-Fuel Ramjet Combustor at Flight-Relevant Conditions. Journal of Propulsion and Energy. 2020. DOI https://doi.org/10.2514/6.2020-3897
[27] Marzouk O, Huckaby D. Simulation of a Swirling Gas-Particle Flow Using Different k-epsilon Models and Particle-Parcel Relationships. Journal of Engineering Letters. 2010;18(1). DOI http://dx.doi.org/10.31219/osf.io/k85nf
[28] Apte S, Mahesh K, Moin P, Oefelein J. Large-eddy simulation of swirling particle-laden flows in a coaxial-jet combustor. Journal of Multiphase Flow. 2003;29(8):1311-1331. DOI http://dx.doi.org/10.1016/S0301-9322(03)00104-6
[29] Waltrup P, White M. History of U.S. Navy Ramjet, Scramjet, and Mixed-Cycle Propulsion Development. Journal of Propulsion and Power. 2002;18(1). DOI https://doi.org/10.2514/2.5928
[34] Yanovskii L, Lempert D, Raznoschikov V, Averkov I. Evaluation of the Performance of Some Metalsand Nonmetals in Solid Propellants for Rocket-Ramjet Engines. combustion Explosion and Shock Waves. 2020;56(1):71-82. DOI 10.1134/S0010508220010098
[35] Xia H, Wang N, Chang Y, Pang J, Wu Y. Influence of Flight Conditions on the Combustion Characteristics of Solid-Fuel Ramjet. Journal of Propulsion and Power. 2025;41(4). DOI https://doi.org/10.2514/1.B39756
