Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization-Reference-Cited by-同舟云学术

Aerodynamic Optimization of a Morphing Leading Edge Airfoil with a Constant Arc Length Parameterization

Published:2018-03 Issue:2 Volume:31 Page:04017093
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Magrini Andrea¹,Benini Ernesto²

Affiliation:

1. Graduate Student, Dept. of Industrial Engineering, Aerospace Engineering, Università Degli Studi Di Padova, Via Venezia 1, 35131 Padova, Italy (corresponding author).

2. Associate Professor, Dept. of Industrial Engineering, School of Engineering, Università Degli Studi Di Padova, Via Venezia 1, 35131 Padova, Italy.

Publisher

American Society of Civil Engineers (ASCE)

Subject

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

Link

http://ascelibrary.org/doi/pdf/10.1061/%28ASCE%29AS.1943-5525.0000812

Reference52 articles.

1. Ahmed M. and Qin N. (2009). “Surrogate-based aerodynamic design optimization: Use of surrogates in aerodynamic design optimization.” 13th Int. Conf. on Aerospace Sciences and Aviation Technology ASAT El Cairo Egypt.

2. Morphing aircraft: The need for a new design philosophy

3. ANSYS FLUENT version 15.0 [Computer software]. ANSYS Inc. Canonsburg PA.

4. A Review of Morphing Aircraft

5. Bettadapura R. Mashburn T. and Crawford R. (2013). “Length-constrained Bézier curve smoothing.” ⟨https://pdfs.semanticscholar.org/b96a/4066a532713d31fcd4e54cfd4e0c1511a0aa.pdf⟩ (Feb. 28 2017).

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