Prediction of Maximum Lift Coefficient of Box-Wing Aircraft through the Combination of an Analytical Adaptation of the DATCOM Method and Vortex-Lattice Simulations-Reference-Cited by-同舟云学术

Prediction of Maximum Lift Coefficient of Box-Wing Aircraft through the Combination of an Analytical Adaptation of the DATCOM Method and Vortex-Lattice Simulations

Published:2022-05 Issue:3 Volume:35 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Cipolla Vittorio¹^ORCID,Abu Salem Karim²^ORCID,Palaia Giuseppe³^ORCID,Binante Vincenzo⁴^ORCID,Zanetti Davide⁵

Affiliation:

1. Assistant Professor, Dept. of Civil and Industrial Engineering, Univ. of Pisa, Via G. Caruso 8, Pisa 56122, Italy (corresponding author). ORCID: .

2. Postdoctoral Fellow, Dept. of Civil and Industrial Engineering, Univ. of Pisa, Via G. Caruso 8, Pisa 56122, Italy. ORCID: .

3. Ph.D. Student, Dept. of Civil and Industrial Engineering, Univ. of Pisa, Via G. Caruso 8, Pisa 56122, Italy. ORCID: .

4. Aeronautical Engineer, Research and Development Dept., SkyBox Engineering Società a Responsabilità Limitata, Via G. Caruso 8, Pisa 56122, Italy. ORCID: .

5. Aeronautical Engineer, Research and Development Dept., SkyBox Engineering Società a Responsabilità Limitata, Via G. Caruso 8, Pisa 56122, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

Mechanical Engineering,Aerospace Engineering,General Materials Science,Civil and Structural Engineering

Link

https://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0001409

Reference27 articles.

1. A Physics-Based Multidisciplinary Approach for the Preliminary Design and Performance Analysis of a Medium Range Aircraft with Box-Wing Architecture

2. Tools and methodologies for box-wing aircraft conceptual aerodynamic design and aeromechanic analysis

3. ACARE (Advisory Council for Aviation Research and Innovation in Europe). 2017. Vol. 1 of Strategic research and innovation agenda (SRIA)—2017 update. Brussels, Belgium: ACARE.

4. Comparison of box-wing and conventional aircraft mission performance using multidisciplinary analysis and optimization

5. Barcala M. C. Cuerno-Rejado S. del Giudice F. Gandía-Agüera and A. A. Rodríguez-Sevillano. 2011. “Experimental investigation on box-wing configuration for UAS.” In Proc. 26th Bristol Int. Unmanned Air Vehicle Systems Conf. Bristol UK: Univ. of Bristol.

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