At 07:51 AM 3/30/2003 -0800, you wrote:
>I have an older Hades that has an Aerodynamic problem I've never been able
>to solve. I'm hoping that may some of you guys that really know this stuff
>could answer the question.
>
>At medium speed the plane will try to nose up if I speed up some. If I start
Okay... now explain how a cheap balsa glider with flat wings flys so well.
You know the type, I think Guillow.
Thanks for the detailed explanation!!!
>From: "Matt Gewain" <[EMAIL PROTECTED]>
>To: "Dana Falconer" <[EMAIL PROTECTED]>, <[EMAIL PRO
>wing at a positive angle of attack
>making the distance over the top of the wing greater and
>the distance on the bottom of the wing less between the
>forward and aft stagnation points. This increases the velocity
>and reduces the pressure over the top of the wing and reduces the
>velocity and in
On 1 Nov 2000 [EMAIL PROTECTED] wrote:
> So this implies that in steady flight there is more air going under
> the LE than coming out at the TE. (Alternatly more air leaving the
> upper surface past TE than entering) Wouldn't that result in
> continuously increasing density under the wing (or vac
On Wed, 01 November 2000, Daniel Olin Miller wrote:
> Let's not perpetuate any misconceptions.
> When the streamlines come back together at the TE, there is no law of man
> or nature that says the particles that were seperated at the LE see each
> other again. In fact, for an airfoil at pos
your input!
>From: Brett Jaffee <[EMAIL PROTECTED]>
>Reply-To: [EMAIL PROTECTED]
>To: Dana Falconer <[EMAIL PROTECTED]>
>CC: [EMAIL PROTECTED]
>Subject: Re: [RCSE] aerodynamic question
>Date: Tue, 31 Oct 2000 19:28:30 -0800
>
>Dana Falconer wrote:
>
> &g
I have always wondered this and I bet all of you out there know the answer.
Okay here goes...
Considering a symmetrical airfoil:
Is a symmetrical airfoil used primarily for aerobatics/inverted flight?
If so doesn't the top of the wing create less pressure therefore helping to
create lift. I
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