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- =Turbofan combustor= [[Category:Turbofan|Combustors]] ...5 KB (914 words) - 00:58, 4 November 2011
- [[Category:Turbofan|Bearings and cooling]] ...6 KB (995 words) - 00:06, 1 October 2013
- ...-spool engine and assess if more stages are required (= more expensive). [[Turbofan:Blades|Blade design and manufacturing]] have a dedicated page. The two pict [[Category:Turbofan|Compressor]] ...7 KB (1,089 words) - 00:47, 28 November 2011
- ...age: [[Turbofan:Compressor|compressor]], [[Turbofan:Turbine|turbine]] or [[Turbofan:Fan|fan]]. In summary, real engines use a fir tree shape to hold the blade ...pressure. We will also use the velocity because the actual work given by a turbofan engine is related to the mass flow rate of the gas expelled by the engine, ...8 KB (1,396 words) - 03:52, 27 November 2011
- ...ork is used to drive both the compressor and the payload. In the case of a turbofan the payload is the fan. Then, the nozzle finishes the expansion and exhaust Let's take an example turbofan engine with a 13cm fan and a 9cm core diameter. The VBPR for this engine is ...11 KB (1,946 words) - 16:52, 10 August 2012
- ...[[:Category:Turbofan|several pages]], with an index at the [[Build a cheap turbofan#Our design propositions|bottom]] of this page. =How to build a cheap (~ $150) turbofan?= ...18 KB (3,022 words) - 01:44, 20 January 2015
Page text matches
- ==Turbofan engine's Mass flow rate calculation== ...4 KB (672 words) - 04:03, 19 November 2012
- ...age: [[Turbofan:Compressor|compressor]], [[Turbofan:Turbine|turbine]] or [[Turbofan:Fan|fan]]. In summary, real engines use a fir tree shape to hold the blade ...pressure. We will also use the velocity because the actual work given by a turbofan engine is related to the mass flow rate of the gas expelled by the engine, ...8 KB (1,396 words) - 03:52, 27 November 2011
- ...[[:Category:Turbofan|several pages]], with an index at the [[Build a cheap turbofan#Our design propositions|bottom]] of this page. =How to build a cheap (~ $150) turbofan?= ...18 KB (3,022 words) - 01:44, 20 January 2015
- =Turbofan combustor= [[Category:Turbofan|Combustors]] ...5 KB (914 words) - 00:58, 4 November 2011
- ...ork is used to drive both the compressor and the payload. In the case of a turbofan the payload is the fan. Then, the nozzle finishes the expansion and exhaust Let's take an example turbofan engine with a 13cm fan and a 9cm core diameter. The VBPR for this engine is ...11 KB (1,946 words) - 16:52, 10 August 2012
- ...-spool engine and assess if more stages are required (= more expensive). [[Turbofan:Blades|Blade design and manufacturing]] have a dedicated page. The two pict [[Category:Turbofan|Compressor]] ...7 KB (1,089 words) - 00:47, 28 November 2011
- ...sts, we'll have to design and build the carrier plane first, including its turbofan engines, which is probably the hardest part of the whole project, and as fa We thus currently focus on the turbofan [[Build_a_cheap_turbofan|research and design]], on which depends everything ...22 KB (3,681 words) - 00:55, 6 November 2017
- ** continuing turbofan operation, '''requires''' more fuel in the aircraft ...6 KB (982 words) - 19:23, 5 November 2012
- * [http://books.google.com/books?id=dZkDQgAACAAJ Turbofan] by Frederic P Miller, Agnes F Vandome and John McBrewster. 2009. ...6 KB (923 words) - 14:04, 31 December 2013
- [[Category:Turbofan|Bearings and cooling]] ...6 KB (995 words) - 00:06, 1 October 2013
