| [1] BALEPIN V. Advances on propulsion technology for high-speed aircraft[J]. High Speed Propulsion Cycles, 2008, 3(2):1-32.
[2] TAGUCHI H, UTAMURA H, SHIMODAIRA K, et al. Design study on hypersonic engine components for TBCC space planes:AIAA-2003-7006[R]. VIRGINIA:AIAA, 2003.
[3] TAGUCHI H, FUTAMURA H, YANAGI R, et al. Analytical study of pre-cooled turbojet engine for TSTO space plane:AIAA-2001-1838[R]. Reston:AIAA, 2001.
[4] 陈大光.高超声速飞行与TBCC方案简介[J].航空发动机, 2006, 32(3):10-13. CHEN D G. Brief introduction of hypersonic flight and TBCC concept[J]. Aeroengine, 2006, 32(3):10-13 (in Chinese).
[5] LONGSTAFF R, BOND A. The SKYLON project:AIAA-2011-2244[R]. Reston:AIAA, 2011.
[6] SATO T, KOBAYASHI H, TANATSUGU N, et al. Development study of the pre-cooler of ATREX engine:AIAA-2003-6985[R]. Reston:AIAA, 2003.
[7] GRAHAM C, HEATH J, CHRISTOPHER A, et al. Analysis of modal growth on the leeward centerplane of the X-51 vehicle:AFRL-RB-WP-TM-2010-3001[R]. Minnesota:AFRL, 2010.
[8] TREFNY C J, ROCHE J M. Performance validation approach for the GTX air-breathing launch vehicle:NASA/TM-2002-211495[R]. Washington, D.C.:NASA, 2002.
[9] PRESTON C, VLADIMIR B, TERRY S, et al. MIPCC technology development:AIAA-2003-6929[R]. Reston:AIAA, 2003.
[10] JUNE K M, JI H J, MAN Y H, et al. High temperature heat exchanger studies for applications to gas turbines[J]. Heat Mass Transfer, 2009, 32(46):175-186. |
CJA
