News Help Institutional access
Back to results
Bibliographic record · Consultation and access
Artículo de revista

Design and Optimization of Aircraft Configuration for Minimum Drag

Zin Win Thu et al · Embry-Riddle Aeronautical University · 2018

Open access available
Quick overview. Review the resource’s basic details, then access the content using the main button. This page shows only the information needed to identify, cite, and open the work.
Author / responsible party
Zin Win Thu et al
Publisher
Embry-Riddle Aeronautical University
Year
2018
ISSN
2374-6793
ISSN
2374-6793
Language
English
Serial publication

3D Printing Technology in Aerospace Industry – A Review

This serial publication contains 428 related contents.
View contents

Resource access

Open the content from the main option or choose another available source.

DOAJ DOAJ Articles
Entrar por DOAJ
Main access

Open access available

Recurso identificado como acceso abierto, sin confirmar automáticamente si es texto completo directo.
Open resource

Summary

Descripción general del contenido del recurso.

<p>This paper presents a reliable and robust optimization for minimum drag of an aircraft at the conceptual design phase. Firstly, the conceptual design code was developed and existing Single Seat Aerobatic (SSA) aircraft was chosen to validate the reliability of developed code. The resulted data from the developed code showed good agreement with the existing data. Secondly, Sequential Quadratic Programming (SQP) optimizer was created and employed as a tool to explore possible aircraft configurations that are more efficient and less costly than an existing design. The optimized results gave lower Drag and better performance.</p>

How to cite

Elegí el formato que necesitás y copiá la referencia al portapapeles.

APA 7

al, Z. W. T. E. (2018). Design and Optimization of Aircraft Configuration for Minimum Drag. https://doi.org/10.58940/2374-6793.1289

MLA

al, Zin Win Thu et. "Design and Optimization of Aircraft Configuration for Minimum Drag." 2018. https://doi.org/10.58940/2374-6793.1289.

Chicago

al, Zin Win Thu et. 2018. "Design and Optimization of Aircraft Configuration for Minimum Drag.". https://doi.org/10.58940/2374-6793.1289.

Harvard

al, Z. W. T. E. 2018, Design and Optimization of Aircraft Configuration for Minimum Drag, Embry-Riddle Aeronautical University, available at: https://doi.org/10.58940/2374-6793.1289 [Accessed 7 Aug. 2026].

Share and print

Save the record, copy its permanent link, or print it as a PDF.

Export reference

You can export the record in common formats for use in a reference manager.

RIS BibTeX

Resource details

Bibliographic information to help confirm that this is the correct material.

Title
Design and Optimization of Aircraft Configuration for Minimum Drag
Author / contributors
Zin Win Thu et al
Publisher
Embry-Riddle Aeronautical University
Publication year
2018
ISSN
2374-6793
ISSN
2374-6793
Language
English

Subjects

Explore related resources through these subjects.

Aeronautical Vehicles; Systems Engineering and Multidisciplinary Design Optimization
Copied