thanks. nice explanation. @goflyprize, if you have Module 12 HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS and can you share these slides or help me where can I find this and similar power point slides? I would be very happy if you could help.
With an increase in torque n angle of attack, you're also increasing drag, therefore you need more power/torque. And of course, too much angle of attack without sufficient power will cause blade stall. Hasta la vista Baby!
"The density of air or atmospheric density, denoted ρ (Greek: rho), is the mass per unit volume of Earth's atmosphere. Air density, like air pressure, decreases with increasing altitude. It also changes with variation in atmospheric pressure, temperature and humidity."
4:41 "You can't do aerodynamics in a vacuum" lool.
That should be the first axiom of aerodynamics
what a lecture
Reading PPT without any physical interpretation and conceptual understanding doesn't make any sense. This can be read in books as well
Greatest Master lecture ever
Great lecture. @goflyprize do you know where I can find the power point slides? It would be incredibly useful.
Hey, @Juan Suarez. Did you get the PowerPoint slides.
thanks. nice explanation. @goflyprize, if you have Module 12 HELICOPTER AERODYNAMICS, STRUCTURES AND SYSTEMS and can you share these slides or help me where can I find this and similar power point slides? I would be very happy if you could help.
With an increase in torque n angle of attack,
you're also increasing drag, therefore you need more power/torque. And of course, too much angle of attack without sufficient power will cause blade stall.
Hasta la vista Baby!
Damn you mentor Duffy, I shouldn't have listened to you
At 17:05, What is "rho" stand for?
"The density of air or atmospheric density, denoted ρ (Greek: rho), is the mass per unit volume of Earth's atmosphere. Air density, like air pressure, decreases with increasing altitude. It also changes with variation in atmospheric pressure, temperature and humidity."
Does anyone have a video walkthrough on how to use Dymore Solutions on a rotorcraft?