-
A. Karabeyoglu, J. Dyer, J. Stevens, and B. Cantwell, “Modeling of N₂O decomposition events,” in Proc. 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conf., Hartford, CT, Jul. 2008, AIAA Paper 2008-4933.
-
B. J. Solomon, Engineering Model to Calculate Mass Flow Rate of a Two-Phase Saturated Fluid Through an Injector Orifice, M.S. report, Dept. Mech. and Aerosp. Eng., Utah State Univ., Logan, UT, USA, 2011.
-
Dyer, J., Doran, E., Dunn, Z., Lohner, K., Bayart, C., Sadhwani, A., Cantwell, B., and Karabeyoglu, A., "Design and Development of a 100 km Nitrous Oxide / Paraffin Hybrid Rocket Vehicle"
-
E. V. Niño and M. R. Razavi, “Design of two-phase injectors using analytical and numerical methods with application to hybrid rockets,” in AIAA Propulsion and Energy 2019 Forum, Indianapolis, IN, Aug. 2019, AIAA Paper 2019-4154. doi: 10.2514/6.2019-4154