Optimization and Performance Analysis of Oleo-Honeycomb Damper Used in Vertical Landing Reusable Launch Vehicle-Reference-Cited by-同舟云学术

Optimization and Performance Analysis of Oleo-Honeycomb Damper Used in Vertical Landing Reusable Launch Vehicle

Published:2018-03 Issue:2 Volume:31 Page:04018002
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Yue Shuai¹,Nie Hong²,Zhang Ming³,Huang Mingyang⁴,Xu Dafu⁵

Affiliation:

1. Ph.D. Candidate, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

2. Professor, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China (corresponding author).

3. Associate Professor, Key Laboratory of Fundamental Science for National Defense-Advanced Design Technology of Flight Vehicle, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

4. Master Candidate, State Key Laboratory of Mechanics and Control of Mechanical Structures, Nanjing Univ. of Aeronautics and Astronautics, Nanjing 210016, China.

5. Senior Engineer, Overall Technology Research Center of Space Transportation System, Shanghai Academy of Spaceflight Technology, Shanghai 201108, 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.1943-5525.0000825

Reference31 articles.

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