AEROBATIC WING LOAD TEST 12Gs

[@novusbuildcraft1400]

How much do the wings weigh?

[@daniela.montenegro2896]

Hola Claudio Felicitaciones!! Muy buen trabajo!! Para que avíon es? Quisiera saber más del proyecto. Tienen otras vías de comunicación, mails, etc? Muchas gracias.

[@claudio767]

Olá Daniel, estou junto com Fernando Zancani, pode continuar se comunicando com Zancani. Boa Sorte

[@castorfan]

Fantastic work. When it will be installed on a 26?.

[@claudio767]

Hello Castor! My apologise to not answer soon, we were talking with a guy in Australia, but his is trying to buy a SU-26 project and buy a wing, but he is planing to get ready in more few years, now we are doing a mold for aileron and elevator

[@onure9135]

can you add the video of the prepearing mold? i want to know how to build a real wing mold

[@claudio767]

Hello! You an check it out at my account on youtube- claudio767 and you can see the is been build.

[@louisvanrijn3964]

It is really a very stiff wing, and problaby very strong. Normally the maximum lift occurs at 12 to 15 degrees angle of attack. Testing a wing had to be done under that angle because the sine of 15 degrees (0.2) works as a forward bending moment in the plane of the wing. Otherwise said, the rear spar is tension loaded by this component. Testing it at zero degrees is wrong, because you have no lift in that condition. A 1th year aviation student knows that.

[@GitoAtom]

Olá Claudio. Onde posso encontrar mais detalhes e contactos da vossa empresa ? Obrigado.

[@claudio767]

Jorge Mota Boa Noite Jorge Mota!A nossa empresa ainda esta bem no inicio, porem no momento estamos no desenvolvimento de uma asa em fibra de carbono na longarina e fibra de vidro no resto.

[@GitoAtom]

claudio767 Seria possível ter um contacto vosso mais directo ? (Facebook ou Email)

[@claudio767]

Ola Jorge Mota. meu email [e-mail]

[@claudio767]

[e-mail]

[@staho9796]

+- 3500Kg ?