Wing Design of an Aircraft - Part 5 | Wing & Airfoil configuration, Wing Volume

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Mastering Up

Mastering Up

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@masteringup
@masteringup 4 жыл бұрын
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.
@arbabraiyan8200
@arbabraiyan8200 3 жыл бұрын
Very quality content..keep it up ma'am. This video deserves much more views..
@narainkarthigeyan8
@narainkarthigeyan8 3 жыл бұрын
Nice presentation..Keep doing👌👌
@masteringup
@masteringup 3 жыл бұрын
Thank you... Kindly keep supporting WINGS OF AERO Team
@raiyaanpanara7892
@raiyaanpanara7892 2 жыл бұрын
at 8:30 how do we got 750 wing loading
@preciousakpata5260
@preciousakpata5260 3 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?
@FahedBelhaj
@FahedBelhaj 8 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?
@gregh3729
@gregh3729 2 жыл бұрын
hi does anyone know where I can find the tables used to choose the wing loading for the uavs
@yubrajkawar8330
@yubrajkawar8330 4 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?
@masteringup
@masteringup 4 жыл бұрын
Its a design thumb rule to find the factor of Cl wing and airfoil.
@charubox
@charubox 4 жыл бұрын
Good
@iAmar10
@iAmar10 Жыл бұрын
Why divide CL of aircraft by 0.9 to get CL of wing?
@samiulhassan9127
@samiulhassan9127 3 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.
@mafketeltje1988
@mafketeltje1988 3 жыл бұрын
Hi hassan, maybe tilt your wing over its axis
@adnan530
@adnan530 4 жыл бұрын
Ma'am what is thumb Rule?
@masteringup
@masteringup 4 жыл бұрын
Thumb rule means standard condition or rule or usually considered. If you have any enquiry feel free to email or contact us.
@adnan530
@adnan530 4 жыл бұрын
@@masteringup Thank you ma'am
@pulakdhara6033
@pulakdhara6033 4 жыл бұрын
Good
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