Further Improvements in the SNUF Blade Design by Numerical Design Optimization Framework-Reference-Cited by-同舟云学术

Further Improvements in the SNUF Blade Design by Numerical Design Optimization Framework

Published:2018-01 Issue:1 Volume:31 Page:04017081
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Eun WonJong¹,Sim JiSoo²,Lee SangWoo¹,Shin SangJoon³

Affiliation:

1. Graduate Student, Dept. of Mechanical and Aerospace Engineering, Seoul National Univ., 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Republic of Korea.

2. Researcher, Korea Aerospace Industries, Ltd., 78, Gongdanro 1-ro, Sanam-myeon, Sacheon, Gyeongsangnam-do 52529, Republic of Korea.

3. Professor, Dept. of Mechanical and Aerospace Engineering, Institute of Advanced Aerospace Technology, Seoul National Univ., 1 Gwanak-ro, Gwanak-gu, Seoul 08826, Republic of Korea (corresponding author).

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.1943-5525.0000794

Reference35 articles.

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3. CATIA [Computer software]. Dassault Systems Vélizy-Villacoublay France.

4. Cesnik C. E. S. Mok J. W. Parikh A. S. and Shin S. J. (2004). “Optimization design framework for integrally twisted helicopter blades.” Proc. 45th AIAA/ASME/ASCE/AHS/ASC Structures Structural Dynamics & Materials Conf. AIAA Palm Springs CA.

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