Selection of High lifting device for your aircraft can be chosen based on the literature study, for an example of fighter aircraft, mostly plain flap are found. now again it depends on the designer with justification.
@arbabraiyan82003 жыл бұрын
Very quality content..keep it up ma'am. This video deserves much more views..
@narainkarthigeyan83 жыл бұрын
Nice presentation..Keep doing👌👌
@masteringup3 жыл бұрын
Thank you... Kindly keep supporting WINGS OF AERO Team
@raiyaanpanara78922 жыл бұрын
at 8:30 how do we got 750 wing loading
@preciousakpata52603 жыл бұрын
How do you get the detail matrix shown at 13:11? I've clicked details using Airfoil Tools, but I just get a series of polar graphs. I've also tried XFoil using the NACA and BEND commands still doesn't produce the information I need. So how should I proceed?
@FahedBelhaj8 ай бұрын
Thank you for your wonderful video😍😍... in the NACA table, we have transport aircraft in the 5-digit column, and since I have a project on transport aircraft, should I use NACA series 5 or 6 in the airfoil database search? And what is the justification for choosing a NACA profile that I can write in my project?
@gregh37292 жыл бұрын
hi does anyone know where I can find the tables used to choose the wing loading for the uavs
@yubrajkawar83304 жыл бұрын
To find coef of lift for wing we divide coef of lift by 0.95 and again for airfoil we divide by 0.90......is this some kind of formula or what?
@masteringup4 жыл бұрын
Its a design thumb rule to find the factor of Cl wing and airfoil.
@charubox4 жыл бұрын
Good
@iAmar10 Жыл бұрын
Why divide CL of aircraft by 0.9 to get CL of wing?
@samiulhassan91273 жыл бұрын
Hello. I really appreciate your effort in this lecture series. I have a simple question. It would mean a lot if you kindly answer it. I am trying to design a small drone. Whose cruise velocity is 26 m/s. and Wing loading is 38 kg/m2. So the cruise lift Coeff. becomes 1.09. As a result, my wing incidence angle becomes 7 deg or 8 deg if I want to produce that desired lift at cruise (keeping the fuselage at 0 deg). What can I do in this situation? Thank you.
@mafketeltje19883 жыл бұрын
Hi hassan, maybe tilt your wing over its axis
@adnan5304 жыл бұрын
Ma'am what is thumb Rule?
@masteringup4 жыл бұрын
Thumb rule means standard condition or rule or usually considered. If you have any enquiry feel free to email or contact us.