참고문헌
- Welland, W.H.M., Brauers, B.M.J. and Vermeulen, E.J., "Future Igniter Technologies," In Space Propulsion Conference, Bordeaux, France, pp. 7-10, May 2010.
- Phillips, B., Pavli, A.J. and Conrad, E.W., "A Resonance Igniter for Hydrogen/Oxygen Combustors," Journal of Spacecraft and Rockets, Vol. 7, No. 5, pp. 620-622, 1970. https://doi.org/10.2514/3.30007
- Marchese, V.P., Rakowsky, E.L. and Bement, L.J., "A Fluid Sounding Rocket Motor Ignition System," Journal of Spacecraft and Rockets, Vol. 10, No. 11, pp. 731-734, 1973. https://doi.org/10.2514/3.61955
- Hartmann, J., "On a New Method for the Generation of Sound Waves," Physical Review, Vol. 20, Issue 6, pp. 719-727, 1922. https://doi.org/10.1103/PhysRev.20.719
- Sprenger, H.S., "Uber Termische Effecte bei Rezonanzrohren," Mitteilungs aus dem Institut fur Aerodynamik, No. 21, pp. 18-35, 1954.
- Avduevskii, V.S., Ivanov, A.V., Karpman, I.M., Traskovskii, V.D. and Yudelovich, M.Ya., "Flow in Supersonic Viscous Under Expanded Jet," Fluid Dynamics, Vol. 5, No. 3, pp. 409-414, 1970. https://doi.org/10.1007/BF01019275
- Abramovich, G.N., Applied Gas Dynamics, Nauka, Moscow, Russia, Part 1, 1991.
- Kessaev, K., Vidal, R. and Niwa, M., "Gas Jet Heat Release Inside a Cylindrical Cavity," International Journal of Heat and Mass Transfer, Vol. 46, No. 10, pp. 1873-1878, 2003. https://doi.org/10.1016/S0017-9310(02)00438-6
- Aref'ev, K.Y., Voronetskii, A.V. and Il'chenko, M.A., "Dynamic Characteristics of a Resonant Gas-Dynamic System for Ignition of a Fuel Mixture," Combustion, Explosion and Shock Waves, Vol. 49, No. 6, pp. 657-661, 2013. https://doi.org/10.1134/S0010508213060038
- Sobieraj, G.B. and Szumowski, A.P., "Experimental Investigations of an Underexpanded Jet from a Convergent Nozzle Impinging on a Cavity," Journal of Sound and Vibration, Vol. 149, No. 3, pp. 375-396, 1991. https://doi.org/10.1016/0022-460X(91)90443-N
- Przirembel, C.E.G. and Fletchert, L.S., "Aerothermodynamics of a Simple Resonance Tube," AIAA Journal, Vol. 15, No. 1, pp. 101-104, 1977. https://doi.org/10.2514/3.60606
- Niwa, M., Santana Jr., A. and Kessaev, K., "Modular Ignition System based on Resonance Igniter," Journal of Propulsion and Power, Vol. 17, No. 5, pp. 1131-1134, 2001. https://doi.org/10.2514/2.5855
- Song, Y.N., Yu, N.J., Zhang, G.Z., Bin, M., Zhou, W.L. and Huang, X., "Investigation of Novel Hydrogen Oxygen Thruster for Orbital Maneuver in Space Station," Chinese Journal of Aeronautics, Vol. 18, No. 4, pp. 289-294, 2005. https://doi.org/10.1016/S1000-9361(11)60247-1
- Yu, N., Cai, G., Zhang, G. and Bin, M., "Experimental Research of Helium Resonance Heating Surface Igniter," 43rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Cincinnati, OH, USA, AIAA 2007-5444, July 2007.
- Sarohia, V., Back, L.H., Roschke, E.J. and Pathasarathy, S.P., "An Experimental Investigation of Fluid Flow and Heating in Various Resonance Tube Modes," NASA JPL, TM 33-780, 1976.
- Marchan, A.R., "Small-Scale Supersonic Combustion Chamber with a Gas-Dynamic Ignition System," Combustion Science and Technology, Vol. 183, Issue 11, pp. 1236-1265, 2011. https://doi.org/10.1080/00102202.2011.589874
- Bouch, D.J. and Cutler, A.D., "Investigation of A Hartmann-Sprenger Tube for Passive Heating of Scramjet Injectant Gases," 41st Aerospace Sciences Meeting and Exhibit, Reno, N.V., USA, AIAA-2003-1275, Jan. 2003.
- Butorin, E.A., Kravtsov, Ya.I., Fiseiskii, V.A., Zaretskii, Ya.V., Mokrousov, G.P. and Chugunov, V.B., "Experimental Study of Gas-Dynamic Ignitor," Translated from Khimicheskoe I Neftyanoe mashinostroenie, No. 7, pp. 9-11, July 1988.