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Search: Posts Made By: da Rock
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Forum: Aerodynamics
10-01-2013, 04:13 PM
Replies: 38
Views: 6,665
Posted By da Rock

That article really shouldn't have tied a...

That article really shouldn't have tied a design's CG location to where the connecting hardware is in a wing. They really have nothing to do with each other. Reading that into any how to article...
Forum: Aerodynamics
10-01-2013, 03:54 PM
Replies: 38
Views: 6,665
Posted By da Rock

Since Bob didn't suggest that making the wing a 3...

Since Bob didn't suggest that making the wing a 3 piece would change any strength, I'd say you aren't missing something there, you're reading in something he didn't even talk about. He simply...
Forum: Aerodynamics
10-01-2013, 12:06 PM
Replies: 38
Views: 6,665
Posted By da Rock

We look forward to seeing what you've decided to...

We look forward to seeing what you've decided to do and how it turns out.

Please be so kind as to show us your progress and tests.

Keep in mind that threads are read by way more people than...
Forum: Aerodynamics
10-01-2013, 02:34 AM
Replies: 38
Views: 6,665
Posted By da Rock

There is a reason I've continued to stress the...

There is a reason I've continued to stress the structural issue instead of the "aerodynamic" one. The issue is not really aerodynamic as much as it's structural, since a successful structure...
Forum: Aerodynamics
09-30-2013, 02:18 PM
Replies: 38
Views: 6,665
Posted By da Rock

Leroy, The Sig wing is designed as a 2 piece. ...

Leroy, The Sig wing is designed as a 2 piece. Use it's design as your guide. The same materials and structure they use to join the 2 halves should work well when you duplicate their joint logic...
Forum: Aerodynamics
09-29-2013, 02:04 AM
Replies: 38
Views: 6,665
Posted By da Rock

The location should be next to the spar for...

The location should be next to the spar for strength. It won't support the primary wing strengthener efficiently unless it's glued to it. The wing designer figured out where to put the spar to...
Showing results 1 to 6 of 6


 
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