Mailing List flyrotary@lancaironline.net Message #58901
From: Ed Anderson <eanderson@carolina.rr.com>
Subject: Re: [FlyRotary] Re: [flyRotary] Spreadsheet Fuel Section
Date: Mon, 27 Aug 2012 09:16:18 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Thanks for the feed back and real-world comparison, Ernest.

I use a 0.55 BSFC figure which may be a bit conservative (gives a higher fuel burn than actual), but I intentionally went conservative in many of those types of choices for the spreadsheet - I figured the builder had excessive optimism that needed to be compensated for {:>)

So the difference may not be in noise of your data but the conservative lean of the spreadsheet.

Ed

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From: "Ernest Christley" <echristley@att.net>
Sent: Sunday, August 26, 2012 11:12 PM
To: "Rotary motors in aircraft" <flyrotary@lancaironline.net>
Subject: [FlyRotary] Re: [flyRotary] Spreadsheet Fuel Section

Ed, I've been trying to calculate my fuel flow and compare that to what the spreadsheet gives.

I'm running four 460cc/min injectors in two banks.  For this paricular log sample, bank1 has pulsewidth of 5.251ms and the second bank is firing for 4.001ms.  With a MAP at 28.5" (96.4kPa) and an intake temp of 91, the engine is spinning 5550RPM with an AFR of 13.1.

Using the fuel flow numbers I have, I should be burning 12.48gph.  The spreadsheet says the number would be 12.8gph.  Given that these data logs have a bit of noise, I call that good nuff' for gubment work.


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