This is a simple question hopefully.
The equation for determining lift produced by an aircraft is the following if I am correct:
L = (1/2) d v2 s CL
If I was designing an aircraft that would maintain flight at standard air pressure at 1000 feet .002308 ISA at 130 MPH with a wing area of...
Hello this is my first post, please let me know if I'm breaking any rules, I'm still a bit hazy on them.
I am in the process of making a permanent magnet induction generator from and old washing machine induction motor. The motor is rated 1725 rmp, 115 volts 6.3 amps at 1/3 horsepower. It is...