Anybody know of any recent testing or comments of wing designs using full span fowler flaps and spoilers?
(The only reports That I've seen is by NACA 1947).
We are about to do flight test with a full scale aircraft with a NACA 23015, 46 ft wing span, chord 60 ". The spoilers are located at 30%...
I have a Czech engine (LOM 337), the engine came with a B-circuit generator, which is not compatible with American
A-circuit voltage regulators, how do I reverse the field on the generator?
I installed a LOM aircraft engine in my plane, the generator supplied is a B-circuit which is not compatible with American A-circuit voltage regulators. How do I reverse the field?