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![]() "Justin Gombos" wrote in message news:NnF8i.1274$Uy4.1025@trndny09... On 2007-06-03, Peter Dohm wrote: There are really three of issues (that I can recall) he 1) A diesel will run on any hydrocarbon fuel that it can pump and meter. 2) Different seals and hoses are compatible with different chemicals--although it would be no surprise to find that all were compatible with biodiesel. 3) Certified aircraft/engines require fuels authorized in the type certificate and/or an STC. 4) Biodiesel supposedly thickens at temperatures that pilots fly in. Though it can be corrected with additives, I would rather have heated wings (thus tanks) to avoid additives and gain de-icing capability for the same feature. Very interesting. Has this been done before, or do de-icers only heat the leading edges of the surface? I am not aware of any present application of heated wings except for transport jets--which I believe are using bleed air. However, there was considerable development work done by NACA during the WWII period. There was at least one report generated involving the use of exhaust gas as the heat source, on a twin engine aircraft, and I don't recall the specifics except that there was concern regarding a loss of heat to one wing in the case of an engine failure. There was also some work done, which was quite promising, regarding the use of the wings of a liquid cooled fighter; which would have provided wing heating as a beneficial side effect. However, whereas the project involved combat aircraft in time of war, the concept was rejected as making the engine cooling system too easy of a target--which was certainly true in that instance. BTW, I believe that the NACA reports are available on the NASA web site. |
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