Hi Guys!
I'm doing a conceptual performance calculation and analysis on co-axial rotor UAV helicopter on hover. However, I'm having conflicting results and if anyone can help me, it would be very great.
The design constant of the helicopter are as follows:
MTOW = 20 kg
κ = 1.15 (Induced Power...
Hi everyone. I'm Usamah from Malaysia. I am a recent graduate in Engineering and currently working as an Aerospace Engineer specifically in design certification.
I have a very high interest in aerospace be it aircraft, helicopter or spacecraft , and my focus area is on the engineering design...