Preliminary Aerodynamic Design Strategy for Prop-Rotors Based on Multifidelity Methods-Reference-Cited by-同舟云学术

Preliminary Aerodynamic Design Strategy for Prop-Rotors Based on Multifidelity Methods

Published:2023-11 Issue:6 Volume:36 Page:
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Zhang Hang¹^ORCID,Zhao Qi-jun²,Zhao Guo-qing³,Wang Bo⁴^ORCID

Affiliation:

1. Ph.D. Candidate, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China. ORCID: .

2. Professor, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China.

3. Lecturer, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China.

4. Lecturer, College of Aerospace Engineering, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, PR China (corresponding author). ORCID: .

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/JAEEEZ.ASENG-4333

Reference27 articles.

1. Bates S. J. J. Sienz and V. V. Toropov. 2004. “Formulation of the optimal Latin hypercube design of experiments using a permutation genetic algorithm.” In Proc. 45th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics & Materials Conf. Reston VA: American Institute of Aeronautics and Astronautics.

2. Schraubenpropeller mit geringstem Energieverlust. Mit einem Zusatz von l. Prandtl;Betz A.;Nachrichten von der Gesellschaft der Wissenschaften zu Göttingen Mathematisch-Physikalische Klasse,1919

3. Capaulson. 2021. “pyKriging.” Accessed August 24 2020. https://github.com/capaulson/pyKriging.

4. Deb K. S. Agrawal A. Pratap and T. Meyarivan. 2000. “A fast elitist non-dominated sorting genetic algorithm for multi-objective optimization: NSGA-II.” In Proc. Int. Conf. on Parallel Problem Solving from Nature 849–858. Berlin: Springer.

5. Aerodynamic shape optimisation of a proprotor and its validation by means of CFD and experiments

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