X-Junk-Score: 0 [] X-Cloudmark-Score: 0 [] X-Cloudmark-Analysis: v=2.3 cv=RZTu9Glv c=1 sm=1 tr=0 a=mUvYIzQhJ/htianyUqExtQ==:117 a=pZ+9jw2XPLJ7kVxgYn3H2A==:17 a=IkcTkHD0fZMA:10 a=x7bEGLp0ZPQA:10 a=CKeqCrOqW6IA:10 a=nTHF0DUjJn0A:10 a=Ia-xEzejAAAA:8 a=7g1VtSJxAAAA:8 a=oDS6_gjrOax6dB4SiCwA:9 a=QEXdDO2ut3YA:10 a=Qa1je4BO31QA:10 a=gvSQh4r-fQ0A:10 a=Urk15JJjZg1Xo0ryW_k8:22 a=grOzbf7U_OpcSX4AJOnl:22 From: "Stephen Izett stephen.izett@gmail.com" Received: from mail-pf1-f179.google.com ([209.85.210.179] verified) by logan.com (CommuniGate Pro SMTP 6.2.14) with ESMTPS id 419526 for flyrotary@lancaironline.net; Thu, 25 Jun 2020 23:41:30 -0400 Received-SPF: pass receiver=logan.com; client-ip=209.85.210.179; envelope-from=stephen.izett@gmail.com Received: by mail-pf1-f179.google.com with SMTP id a127so4045724pfa.12 for ; Thu, 25 Jun 2020 20:41:32 -0700 (PDT) DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=gmail.com; s=20161025; h=from:content-transfer-encoding:mime-version:subject:date:references :to:in-reply-to:message-id; bh=6djcrIDhfqe33ykGIHvVfIF4eLmzKhtFqzwWva12dVI=; b=hMVtfKEj/UoXvtwdmlp5h1Rp3CcMCQOdWtVG21GDYot/YP2bcyEsBniwaG27zML9Vh f4tVS987XJJLUPNaq6zh/wpnmEYdTurIKUEJpTjlsWffqkxAJHrXvrZ3rxe7Vly9OL+x moL+RhxRZ3Tb13Gs2mGwABAobps+dSJZGgcc5dFZQv77TgWYHXuZj99JpokGQkcGsxV2 HzbMnJ3cPPzIz7foGus8BAQO+cxAEnhUxe+kOU6vluTT6lPn5jnU5jpUqh/RWvKVTgKK Fqr+SdhBHo2jgUkMs8kbg8XWfheYknh0PJRu3EXcMkabp8+osyfPlenK6crYZppoWBFE JQSw== X-Google-DKIM-Signature: v=1; a=rsa-sha256; c=relaxed/relaxed; d=1e100.net; s=20161025; h=x-gm-message-state:from:content-transfer-encoding:mime-version :subject:date:references:to:in-reply-to:message-id; bh=6djcrIDhfqe33ykGIHvVfIF4eLmzKhtFqzwWva12dVI=; b=ioMnLx8PyMvA9m8fB48xrZtTYbFYJi5Wvp7AvCWeVDR1D5A9YPJ7+lSbfJUDW/mcK5 IbgpORxo7htG3tjyNlYIDgXO99a/5slccqOJStIvyA0vVUdFymF6MMwwMkf/XnaSw56i Mu2bTVVUlWfM2s0AdCnkeGfS88KZQOHv8zct4XOCv081uV3hJ5dkJCfoZGdQaM6a3E78 +eiEF6IfPkIwSccp0m98hhle8KQiVlCKno/Vk71n/rzDo0Limv4z7KEbSzKidTbwds4C Ij7Yq6v1pApwOBJ7yrVaViNNZcjWlnYjlJBGUMQIvt+CELS8M0TcOWdBUTC3SFmyeJAS bUYw== X-Gm-Message-State: AOAM533oF9SaoBJt7+SWQKTVBwoPEOycvKVaTNZ/R3rauMJ5PiQOjR6Q /yRs8djQRiuVrwYyfXjGmxHTEBWl X-Google-Smtp-Source: ABdhPJy98KnTNnrUcrKXaoObO96fVbB9OmUdgpn5OKm54ULY+dXF5ZgQWbXUNhCTIlM4VIIcqYpS+Q== X-Received: by 2002:aa7:99d0:: with SMTP id v16mr833646pfi.98.1593142874031; Thu, 25 Jun 2020 20:41:14 -0700 (PDT) Return-Path: Received: from macbook-pro.lan (203-59-74-185.perm.iinet.net.au. [203.59.74.185]) by smtp.gmail.com with ESMTPSA id u24sm20959491pga.47.2020.06.25.20.41.11 for (version=TLS1_2 cipher=ECDHE-ECDSA-AES128-GCM-SHA256 bits=128/128); Thu, 25 Jun 2020 20:41:13 -0700 (PDT) Content-Type: text/plain; charset=utf-8 Content-Transfer-Encoding: quoted-printable Mime-Version: 1.0 (Mac OS X Mail 12.4 \(3445.104.11\)) Subject: Re: [FlyRotary] BSFC change on staging Date: Fri, 26 Jun 2020 11:41:09 +0800 References: To: Rotary motors in aircraft In-Reply-To: Message-Id: <907F7F45-3279-4735-8975-9B9BDF6C1AEF@gmail.com> X-Mailer: Apple Mail (2.3445.104.11) Hi there Steve Thanks for your work here.=20 How do you measure the BSFC? So you have a version of the EC software where you can still change the = Staging point MAP. The BSFC is ~0.5 better unstaged. Is this due to better fuel-air mixing = or is something else at play? Am I right in thinking that at an economy cruise, a BSFC change of 0.5 = might yield an approx 0.9G/hr ($5/hr) of fuel saving. That might then argue for a Staging Point at the earlier 15.5=E2=80=9D = MAP to enable unstaged cruise rather than the locked in 20=E2=80=9D MAP = of the current software version. What is your thoughts and conclusion if you have reached any? Thanks again Steve Steve Izett > On 26 Jun 2020, at 8:47 am, Steven W. Boese SBoese@uwyo.edu = wrote: >=20 > 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. >=20 > Steve Boese=20 > -- > Homepage: http://www.flyrotary.com/ > Archive and UnSub: = http://mail.lancaironline.net:81/lists/flyrotary/List.html