共 19 条
- [1] ZOU Bowen, XU Quanhong, CAO Wenyu, Et al., Lean blowout mechanism of coupled recirculation zone in concentric staged combustor, Journal of Aerospace Power, 28, 8, pp. 1759-1763, (2013)
- [2] ZHAO Jiangxing, Pollutant emission and development of low-emission combustion technology for civil aero engine, Journal of Aerospace Power, 23, 6, pp. 986-996, (2008)
- [3] YI T, GUTMARK E., Lean blowout features and control in a swirl-stabilized, partially premixed gas turbine combustor, 44th AIAA Aerospace Sciences Meeting and Exhibit, (2006)
- [4] EGGLESS R L G, BROWN C T., Comparison of numerical and experimental results of a premixed DLE gas turbine combustor, (2001)
- [5] MICHAEL F,, DOUG T,, RICHARD S,, Et al., Development of the GE aviation low emissions TAPS combustor for next generation aircraft engines, 50th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, (2012)
- [6] FOUST M,, THOMSEN D, Et al., Development of the GE aviation low emissions TAPS combustor for next generation aircraft engines, AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, (2012)
- [7] LAZIK W,, DOERR T,, BAKE S,, Et al., Development of lean-burn low-NOx combustion technology at Rolls-Royce Deutschland, (2008)
- [8] pp. 324-336, (2005)
- [9] LIU Jing, ZHAO Junwu, Development of low emission combustor for foreign civil aeroengine, Aeroengine, 38, 4, pp. 11-16, (2012)
- [10] pp. 128-132, (1988)