Mailing List flyrotary@lancaironline.net Message #4104
From: <echristley@nc.rr.com>
Subject: Re: [FlyRotary] cooling air flow path (was:Re: EWP check valves)
Date: Thu, 23 Oct 2003 15:21:51 -0400
To: Rotary motors in aircraft <flyrotary@lancaironline.net>

You mentioned the exit path as near the end of the turtleback. Is this on a Dyke Delta? I don't know about the Delta, but on most conventional airframes the top of the fuse. behind the canopy is actually a *high* pressure area. Have you checked this out with the designer of the airframe?
Charlie
former owner of a Thorp T-18, a design that has the cockpit fresh air input cut into the *back* of the canopy.



The Delta is a flying wing design, ie the fuselage is airfoil shaped and actually carries 1/3 of the air load.  My assumption was that as an airfoil, it would have airfoil characteristics.  NACA studies indicated that the lowest pressure point on an airfoil was at the 70% MAC point.



Subscribe (FEED) Subscribe (DIGEST) Subscribe (INDEX) Unsubscribe Mail to Listmaster