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On Sep 7, 6:45*am, Peter Higgs wrote:
Perhaps the best initial solution would be to drill a 10-15mm hole in the access cover, (or anywhere else really.) which depending upon the airflow, would act as a static vent... *neither increasing or decreasing the ambient pressure. On Sep 7, 6:45 am, Peter Higgs wrote: Perhaps the best initial solution would be to drill a 10-15mm hole in the access cover, (or anywhere else really.) which depending upon the airflow, would act as a static vent... neither increasing or decreasing the ambient pressure. I'm not sure I would want an "air spigot" pointing straight out of the fuselage into the airstream - seems like unnecessary drag versus a solution that lines the flow up with the external slipstream. The reverse NACA duct has been shown to work well and it's my understanding that it even produces a small amount of thrust. As to altimeter readings - my altimeter is hooked to my tailboom static ports. I'd recommend it as a general practice if you have external ports available. My feeling is that any solution that vents high-pressure fuselage air would yield a more accurate altimeter reading than not venting but that the differences in any even aren't that large. 9B |
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