Mailing List flyrotary@lancaironline.net Message #38603
From: Al Gietzen <ALVentures@cox.net>
Subject: RE: [FlyRotary] Oil cooler inlet
Date: Fri, 20 Jul 2007 21:23:58 -0800
To: 'Rotary motors in aircraft' <flyrotary@lancaironline.net>

Whatever the gear well covers do I don’t know.  I have 9.5” steady H2O ram pressure in front of the middle of the scoop, 5/8” below the underwing surface; and that’s plenty adequate.

 

Al

 

Subject: [FlyRotary] Oil cooler inlet

 

Al,

 

I'm in agreement with TJ on this one. Tuft test is definitely in order. I did not realize that the gear door and wheel fairing were where they are. Even if the transition is fairly smooth, the opening at the wheel and the gaps in the door are going to make a mess in the area aft of the door. Think little jets of air from all the gaps. This will trip the boundary layer and make it much thicker than normal. It would have to be fully sealed (air tight) around the gear door to stop this.

 

Any high pressure that the open wheel well develops will squirt out around the door.

 

I would test to see how bad the flow is loused up around the gear door with some oil or tufts. You may find that sealing the fairing up improves things a lot.

 

Sealing the gap around the cooler certainly can't hurt things.

 

Interested to see how the VG's and gap seal improve things.

 

Armchair QB in action here ;-)

 

Monty

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