Platform for Transport Aircraft Wing–Body Parametric Modeling and High-Lift System Design-Reference-Cited by-同舟云学术

Platform for Transport Aircraft Wing–Body Parametric Modeling and High-Lift System Design

Published:2017-09 Issue:5 Volume:30 Page:06017004
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Tian Yun¹,Qu Xiangnan²,Liu Peiqing³,Yan Shiwei⁴

Affiliation:

1. Lecturer, National Laboratory for Aeronautics and Astronautics, Beihang Univ., Beijing 100191, People’s Republic of China.

2. Master, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, People’s Republic of China.

3. Professor, School of Aeronautic Science and Engineering, Beihang Univ., Beijing 100191, People’s Republic of China (corresponding author).

4. Dept. of Surface Ship, China Marine Development and Research Center, Beijing 100164, People’s Republic of China.

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.1943-5525.0000761

Reference14 articles.

1. CADS [Computer software]. Open Mind Technologies AG Wessling Germany.

2. Lu X. L. and Gong X. D. (2008). “Development research of aircraft synthetic conceptual design software.” Third Chinese Society of Aeronautics and Astronautics Youth Science and Technology Forum Chinese Society of Aeronautics and Astronautics Beijing 3–14.

3. Manning T. A. et al. (2004). “ComGeom2: A geometry tool for multidisciplinary analysis and data sharing.” 10th AIAA/ISSMO Multidisciplinary Analysis and Optimization Conf. AIAA-2004-4303 American Institute of Aeronautics and Astronautics Albany NY.

4. OpenCADS [Computer software]. Open Mind Technologies AG Wessling Germany.

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