Erratum for “Flutter of a Swept Aircraft Wing with a Powered Engine” by A. Mazidi and S. A. Fazelzadeh

Mazidi, A.; Fazelzadeh, S. A.

doi:10.1061/(ASCE)AS.1943-5525.0000159

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Dec 15, 2011

Erratum for “Flutter of a Swept Aircraft Wing with a Powered Engine” by A. Mazidi and S. A. Fazelzadeh

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Authors: A. Mazidi and S. A. FazelzadehAuthor Affiliations

Publication: Journal of Aerospace Engineering

Volume 25, Issue 1

https://doi.org/10.1061/(ASCE)AS.1943-5525.0000159

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The following corrections should be made to the original paper:

1.

On page 245, Eq. (15) should be

L = π ρ_{\infty} b^{2} [- \ddot{w} + U_{\infty} \cos Λ \dot{θ} - U_{\infty} \sin Λ {\dot{w}}^{'} - b a (\ddot{θ} + U_{\infty} \sin Λ {\dot{θ}}^{'})] + 2 π ρ_{\infty} U_{\infty} b \cos Λ [- \dot{w} + U_{\infty} \cos Λ θ - U_{\infty} \sin Λ w^{'} + b (\frac{1}{2} - a) (\dot{θ} + U_{\infty} \sin Λ θ^{'}) - λ_{0}]

2.

On page 246, Eq. (16) should be

M = - π ρ_{\infty} b^{3} [\frac{1}{2} (U_{\infty}^{2} \sin Λ \cos Λ θ^{'} + U_{\infty} \cos Λ \dot{θ}) - U_{\infty} \cos Λ a \dot{θ} + a \ddot{w} + U_{\infty} \sin Λ a {\dot{w}}^{'} + b (\frac{1}{8} + a^{2}) (\ddot{θ} + U_{\infty} \sin Λ {\dot{θ}}^{'})] - 2 π ρ_{\infty} \cos Λ b^{2} (\frac{1}{2} + a) [\dot{w} - U_{\infty} \cos Λ θ + U_{\infty} w^{'} \sin Λ - b (\frac{1}{2} - a) (\dot{θ} + U_{\infty} \sin Λ θ^{'}) + λ_{0}]

3.

On page 246, Eq. (23) should be

{q} = {q_{1}^{T} q_{2}^{T} λ^{T}}^{T}

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Journal of Aerospace Engineering

Volume 25 • Issue 1 • January 2012

Pages: 149

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Received: Jul 6, 2011

Accepted: Sep 8, 2011

Published online: Dec 15, 2011

Published in print: Jan 1, 2012

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A. Mazidi

Ph.D. Candidate, Dept. of Mechanical Engineering, Shiraz Univ., Shiraz, Iran. E-mail: [email protected]

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S. A. Fazelzadeh

Associate Professor, Dept. of Mechanical Engineering, Shiraz Univ., Shiraz, Iran (corresponding author). E-mail: [email protected]

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Erratum for “Flutter of a Swept Aircraft Wing with a Powered Engine” by A. Mazidi and S. A. Fazelzadeh

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