Mailing List flyrotary@lancaironline.net Message #65951
From: Steven W. Boese SBoese@uwyo.edu <flyrotary@lancaironline.net>
Subject: BSFC change on staging
Date: Fri, 26 Jun 2020 00:47:46 +0000
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
I ran a test on my engine stand with staged and unstaged fuel injectors but with the same fuel flow and MAP.  The results are shown in the attached image.  The engine is a 2010 2nd generation Renesis 6 port from an automatic transmission car with the high RPM ports blocked off and stock fuel injectors.  The reduction drive ratio is 3.18:1.  The prop is a 3 blade 72" Warp Drive and was operating just below stalled RPM.  A turbo is installed but no boost was used in the test.  No attempt was made to operate at minimum BSFC.

Steve Boese 
Attachment 
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