1. Bartz, D. R., A Simple Equation for Rapid Estimation of Rocket Nozzle Convective Heat Transfer Coefficients, Jet Propul., Vol.27, No.1 (1957), pp.49–51.
2. Chen, X., Ma, D. and Yang, V., High-Fidelity Numercial Simulations of Impinging Jet Atomization, 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit (2012), AIAA-2012-4328.
3. Daimon, Y. et al., Flow Field and Heat Transfer Analysis in a MON/MMH Bipropellant Rocket Engine, International Journal of Energetic Materials and Chemical Propulsion, Vol.16, Issue 3 (2017), pp.263–280.
4. Dambach, E. M., et al., Investigation into the Hypergolic Ignition Process Initiated by Low Weber Number Collisions, Journal of Propulsion and Power, Vol.29, No.2 (2013), pp.331–38.
5. Davis, S. M. and Yilmaz, N., Advances in Hypergolic Propellants: Ignition, Hydrazine, and Hydrogen Peroxide Research, Advances in Aerospace Engineering 2014 (2014), pp.1-9.