Aircraft wing structural design application in MATLAB App Designer

• Autorzy: Bilal Ahmed , Siddiqui Faisal , Abbas Messam , Mansoor Mohtashim

Identyfikatory

DOI

10.7494/cmms.2021.4.0762

• Języki publikacji: EN

Abstrakty

EN

This study focuses on developing an automated application in the MATLAB® App Designer module, based on basic structural members and different theories for various loading cases, providing ballpark values of bending and torsional stiffness and sizing of the load-carrying structural member at a span wise location. All the code developed on MathWorks (2018) is automated using the App Designer module. In this approach, governing equations of structural members under different types of loading are solved in MATLAB IDE with the assumption that in the preliminary phase MATLAB App Designer provides an easy drag and drop type application developer that can be easily subsumed in any mathematical automation process.

Słowa kluczowe

EN

automated aircraft wing design; aircraft preliminary design phase; wing structure; analytical method; bending; torsional stiffness; MATLAB App Designer

• Wydawca: Wydawnictwa AGH
• Czasopismo: Computer Methods in Materials Science
• Rocznik: 2021
• Tom: Vol. 21, No. 4
• Strony: 193--202
• Opis fizyczny: Bibliogr. 13 poz., rys.

Twórcy

autor

Bilal Ahmed

• Department of Aerospace Engineering, Air University A&AC Campus Islamabad, Pakistan

• https://orcid.org/0000-0002-5502-8559

autor

Siddiqui Faisal

• Department of Aerospace Engineering, Air University A&AC Campus Islamabad, Pakistan

autor

Abbas Messam

• Department of Aerospace Engineering, Air University A&AC Campus Islamabad, Pakistan

autor

Mansoor Mohtashim

• Department of Aerospace Engineering, College of Aeronautical Engineering, NUST, Risalpur Pakistan

Bibliografia

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• Giles, G.L. (1994). Design-oriented structural analysis. In: B.H.V. Topping, M. Papadrakakis (Eds.), Advances in Structural Engineering Computing (pp. 1–10). Civil-Comp Press, https://www.doi.org/10.4203/ccp.29.1.1.
• MathWorks (2018). Documentation. MATLAB The Language of Technical Computing, https://www.mathworks.com/help/matlab/.
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• Niu M.C.-Y. (2001). Airframe Stress Analysis and Sizing (2nd ed.). Adaso Adastra Engineering Center.
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• Youhua, L. (2000). Efficient Methods for Structural Analysis of Built-Up Wings [unpublished dissertation]. Virginia Polytechnic Institute and State University.
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Uwagi

Opracowanie rekordu ze środków MEiN, umowa nr SONP/SP/546092/2022 w ramach programu "Społeczna odpowiedzialność nauki" - moduł: Popularyzacja nauki i promocja sportu (2022-2023).