T.J.
Registered User
Alaska
This topic has been discussed before, and I read all the responses, but, I have a few questions.
I did a Google search and read most of the information I received. Most of the wind tunnel test and research done on Gurney flaps were done on "go fast" planes. I'm not really interested in increased lift on a Cub wing in level flight. I'm interested in slow flight, as in when landing.
1. What does it do when installed on the Cub flap when it is deployed?
2. Does it give more roll control if it is installed on the ailerons?
3. Would it give you more pitch control if they were installed on the elevators?
All comments are welcome. Thanks.
I did a Google search and read most of the information I received. Most of the wind tunnel test and research done on Gurney flaps were done on "go fast" planes. I'm not really interested in increased lift on a Cub wing in level flight. I'm interested in slow flight, as in when landing.
1. What does it do when installed on the Cub flap when it is deployed?
2. Does it give more roll control if it is installed on the ailerons?
3. Would it give you more pitch control if they were installed on the elevators?
All comments are welcome. Thanks.