Thanks. I finally get it. My teacher keeps taking random parts out of books, randomly changing up the notation in the equations and translating to dutch and back (so it's harder to look up the original soruce).
Interesting about the relation between the drag to the cross-section. That mean that the angle off attach is affecting the cross-section, which finally will affect the drag. Will you please explain it more? Should I project it? If I have to project, where should be the projection? To the plane direction, or to the wind resultant (relative) direction?
Hey could you help me please I want to calculate Cx and Cz (drag and lift coefficient) of a 46m/s wind speed at an inclined panel with 30° incidence angle the force should be daN/m² or we could calculate the Drag and lift force on a panel of a 1.7x1 = 1.7m² area. SEARCHING SINCE A WEEK BUT NOTHING FOUND ON INTERNET. MECAFLUX software GIVES An automatic RESULT BUT I couldn't calculate manually.
The authors have two wrong scientific approaches: researching the creation of Lift force and Low pressure at upper side of the wing, relative to the ground surface and Earth. I explain the aerodynamic cavitation and existence of Lee side aerocavern, and creation of Aerodynamic force.
Thanks. I finally get it. My teacher keeps taking random parts out of books, randomly changing up the notation in the equations and translating to dutch and back (so it's harder to look up the original soruce).
Thank you , you saved me
Interesting about the relation between the drag to the cross-section. That mean that the angle off attach is affecting the cross-section, which finally will affect the drag. Will you please explain it more? Should I project it? If I have to project, where should be the projection? To the plane direction, or to the wind resultant (relative) direction?
What's the difference between upthrust and lift ?
Hey could you help me please I want to calculate Cx and Cz (drag and lift coefficient) of a 46m/s wind speed at an inclined panel with 30° incidence angle the force should be daN/m² or we could calculate the Drag and lift force on a panel of a 1.7x1 = 1.7m² area. SEARCHING SINCE A WEEK BUT NOTHING FOUND ON INTERNET. MECAFLUX software GIVES An automatic RESULT BUT I couldn't calculate manually.
Is that "minus" one half in the equation or just one half?
That pen is good. Can i know the name? Btw nice video simple and decent
Voldemort is back :p
I love old comments.
Are you from New Zealand sir
Dragon Lift!!! Cool
The authors have two wrong scientific approaches: researching the creation of Lift force and Low pressure at upper side of the wing, relative to the ground surface and Earth. I explain the aerodynamic cavitation and existence of Lee side aerocavern, and creation of Aerodynamic force.
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