Great article for everyone...thanks
Darryl DuRossette
On Fri, Oct 14, 2011 at 11:53 AM, Kenneth B. Jones
wrote:
> Rudi,
>
> "Vne" is marked as IAS (based on having a calibrated airspeed indicator).
> But before you go too fast at high altitude, please read
> http://vansaircraft.com/pdf/hp_limts.p
Isn't 18,000' the base of class A airspace with the requirement of IFR panel
and pilot?
DC
Bothell, WA
>
>From: Rudi Venter
>To: KRnet
>Sent: Friday, October 14, 2011 10:18 AM
>Subject: Re: KR> Vne/Flutter
>
>On 10/14/20
On 10/14/2011 6:53 PM, Kenneth B. Jones wrote:
> Rudi,
>
> "Vne" is marked as IAS (based on having a calibrated airspeed indicator).
>
> But before you go too fast at high altitude, please read
> http://vansaircraft.com/pdf/hp_limts.pdf . It's very enlightening.
>
> Ken Jones
Thanks Ken!
The Van
Rudi,
"Vne" is marked as IAS (based on having a calibrated airspeed indicator).
But before you go too fast at high altitude, please read
http://vansaircraft.com/pdf/hp_limts.pdf . It's very enlightening.
Ken Jones
- Original Message -
From: "Rudi Venter"
To: "'KRnet'"
Sent: Frid
I would also add that Vne is normally expressed as the speed at which when the
airspeed is increased beyond that speed , that the airfoil has the capability
to produce loads that exceed the aircraft's ability to with stand. Simply
stated, the wing can generate more lift than the spars can hold.
The maximum velocities allowed are Va in turbulent air and Vne in smooth air
conditions.
Your aircrafts Vne is an indicator of speed, in smooth air conditions, where
permanent distortion or control flutter may occur. As stated, you can fly
at Vne in safety, but you cannot expect to make sudden ma
At 10:16 AM 7/3/04 -0500, you wrote:
>The maximum velocities allowed are Va in turbulent air and Vne in smooth air
>conditions.
>Your aircrafts Vne is an indicator of speed, in smooth air conditions, where
>permanent distortion or control flutter may occur. As stated, you can fly
>at Vne in safety
Colin and Bev wrote:
"I would also add that Vne is normally expressed as the speed at which when
the airspeed is increased beyond that speed , that the airfoil has the
capability to produce loads that exceed the aircraft's ability to with stand
"
While this once was true for early aircraft design
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