MuckundSharma
Mechanical Engineer
University of Waterloo · BASc Mechanical Engineering
Driven to advance
and redefine
the next era of flight.
Angle of attack
0.0°
Lift coefficient (idealised)
0.31
Idealised flow: no drag or stall, so lift keeps climbing. Real wings stall.
Keep scrolling to pitch the wing up. MX-01 write-up →
Let's talk about what you're building.
I'm available for co-op roles in aerospace, structures, and mechanical design.