User contributions for Vincent
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27 November 2011
- 01:2901:29, 27 November 2011 diff hist +136 N File:Blade nomenclature.png Nomenclature of aerofoils (used in fan/compressor/turbine blades). Source is the chapter "2.0 Axial-Flow Compressors" from M. P. Broyce. current
- 01:2801:28, 27 November 2011 diff hist +242 Turbofan:Compressor adding broyce link
17 November 2011
- 03:3503:35, 17 November 2011 diff hist +58 User:Vincent little user page update
- 03:3203:32, 17 November 2011 diff hist −44 Founder Redirected page to User:Vincent current
16 November 2011
- 12:1412:14, 16 November 2011 diff hist +177 Join →How to join?: account request
- 12:0612:06, 16 November 2011 diff hist +244 Main Page →N-Prize and reflections on low-cost access to space: otaski update
15 November 2011
4 November 2011
- 00:5800:58, 4 November 2011 diff hist +1,888 Turbofan:Combustors →Our design: sections draft current
3 November 2011
- 23:4123:41, 3 November 2011 diff hist +125 Turbofan:Combustors →Typical designs: text fixes
2 November 2011
- 20:1320:13, 2 November 2011 diff hist +488 Turbofan:Combustors →Our design: sketch of the combustor
- 20:0820:08, 2 November 2011 diff hist +118 N File:Combustor sketch section.jpg Sketch of the combustor cross-section. The green part is the shaft, the transparent light blue part is the core shell. current
- 20:0020:00, 2 November 2011 diff hist +959 Turbofan:Alternative Designs →Full transonic engine design in a single spool with 2.1 BPR: images
- 19:3619:36, 2 November 2011 diff hist +140 N File:Engine core and fan.jpg Sketch of the engine, with the core and the fan duct, aft-mounted fan and first stage compressor rotor drafted. The chamber is in red/brown. current
- 19:3519:35, 2 November 2011 diff hist +140 N File:Engine core and fan side.jpg Sketch of the engine, with the core and the fan duct, aft-mounted fan and first stage compressor rotor drafted. The chamber is in red/brown. current
1 November 2011
- 22:3822:38, 1 November 2011 diff hist +879 Turbofan:Combustors flow properties
- 22:2922:29, 1 November 2011 diff hist +1,810 Turbofan:Combustors first draft
- 22:0622:06, 1 November 2011 diff hist +135 Resources →Turbines and turbofans: klaus97
- 00:1900:19, 1 November 2011 diff hist +363 Turbofan:Alternative Designs →Full transonic engine design in a single spool with 2.1 BPR: reading again and corrections
31 October 2011
- 23:3523:35, 31 October 2011 diff hist +2,557 Turbofan:Alternative Designs transonic design
- 21:2821:28, 31 October 2011 diff hist +555 Turbofan:Alternative Designs vbpr