A Study on the igniter using resonance tube |
Lee, Jung-Min
(모스크바항공대 로켓엔진학과)
Kwon, Min-Chan (모스크바항공대) Shin, Dong-Sun (한국항공우주연구소) Semenov, V.V. (모스크바항공대 로켓엔진학과) |
1 | Kunthov V.M., Ostrohova S.I. Filipkov K.N. Pressure oscillation and gas heating in flow of supersonic jet to cylindrical hole. Mechanics of fluid and gas, 1977, N5. |
2 | Lee Jungmin, Semenov V.V. Gasdynamic heater, Russian Patent No. 2225574, March 10, 2004. |
3 | 이택상,신완순,박종호,김윤곤 "충격파 간섭에 따른 초음속 충돌제트의 실험 연구" 한국항공우주학회지, 제29권 4호, pp1-7, 2001. |
4 | Lee Jungmin, Semenov V.V., Ivanov I.E. Increase of efficiency in gasdynamic igniter for unselfignited fuel. 12th International Conference on computational mechanics and modern applied software systems, 2003, Vladimir, Russia. |
5 | Lee Jungmin. Semenov V.V., Ivanov I.E., Kryukov I.A. Improvement of effect of gasdynamic igniter for unselfignited fuel. 54th international astronautical congress of IAF, 2003, Bremen, Germany. |
6 | Hartmann, J., On the production of acoustic waves by means of an air-jet of a velocity exceeding that of sound, the Philosophical magazine, Vol. 11, 1931, pp. 926-948. DOI |
7 | Sergienko A.A., Semenov V.V. Gasdynamic igniter. Aviational Technics. 2000. N2, pp.44-47. |
8 | Phillips B.R., Pavel A.J. Resonance tube ignition of hydrogen oxygen mixtures. NASA TND-6354 1971, Nrd-6354. |
9 | Sprenger H.S., On Thermal Effects in Resonance Tube. Mittelung aus dem Inst. fur Aerodynamik, ETH, Zurich, 1954, Nr21. |
10 | Eliseev Yu.B., Cerkez A.Ya. Effect of improvement of stagnation temperature in gas flow to deep hole. Mechanics of fluid and gas, 1971, N5. |
11 | Ivanov I.E., Kryukov I.A. Oscillation mode of flow in gasdynamic igniter. Mathematical modeling 1999. vol 11. N2. |