Assignment no. 10

Utkarsh Patel

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Apr 1, 2024, 8:30:38 AM4/1/24

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1. The given CL(alpha) of wing and tail is of 2D(airfoil) or 3D(wing) ??

2. To get VH, is it assumed from historical data (VH~0.5 to 0.7) OR the moment arm is to be calculated assuming X(cg) = X(ac)w ??

This explanation is needed in order to solve all the questions of the Assignment 10.

Nikhil Balakrishnan

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Apr 1, 2024, 9:58:57 AM4/1/24

to Discussion forum for Aircraft Design, Utkarsh Patel

Hi sir,
exactly the doubt i had asked previously. Lt= Xcg-Xac of tail. As Xcg is not given, can we assume the Vh to be 0.7 just like the lectures

NOC24 AE02

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Apr 18, 2024, 1:10:36 AM4/18/24

to Discussion forum for Aircraft Design, nikhi...@gmail.com, utkarsh...@gmail.com

Dear Candidate,

Please see the solution of assignment 10.

Thank you.

NOC24 AE02

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Apr 18, 2024, 1:10:42 AM4/18/24

to Discussion forum for Aircraft Design, utkarsh...@gmail.com

Dear Candidate,

Please see the solution of assignment 10.

Thank you.

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