Ernest,
The procedure is to test with many steps increasing
speed in small increments always ready
to reduce throttle and increase AOA at the
slightest indication of flutter..............
Kelly Troyer
"DYKE DELTA JD2" (Eventually)
"13B ROTARY"_ Engine
"RWS"_RD1C/EC2/EM2
"MISTRAL"_Backplate/Oil
Manifold
"TURBONETICS"_TO4E50 Turbo
From: Ernest
Christley <echristley@att.net>
To: Rotary motors in aircraft <flyrotary@lancaironline.net>
Sent: Sunday, July 3, 2011 2:11
PM
Subject: [FlyRotary] Re:
GSL393/74028 Fuel Pump Replacement/Fuel Leak
On 07/02/2011 11:12 AM, Thomas Mann wrote:
I know that the plans built composite aircraft (Rutan designs and
derivatives) can have a Vne that can be higher or lower than the design
specs as a direct result of workmanship. Each (in my case a Long-EZ)
aircraft is a one-off and only flight testing can determine the TRUE
V-speeds.
I think that is less of a factor in the RV world but a factor just
the same.
Flutter is really ugly.
How is the Vne testing
performed? I can't think of anything other than pushing the throttle
to the firewall and waiting to see what happens, but that sounds awful
dangerous to
me.