Efficient Analysis of HALE Aircraft Structure for Static Aeroelastic Behavior-Reference-Cited by-同舟云学术

Efficient Analysis of HALE Aircraft Structure for Static Aeroelastic Behavior

Published:2017-01 Issue:1 Volume:30 Page:04016075
ISSN:0893-1321
Container-title:Journal of Aerospace Engineering
language:en
Short-container-title:J. Aerosp. Eng.

Author:

Liu Lu¹,Kim Taehyoun²,Lai Kwok Leung³

Affiliation:

1. Ph.D. Candidate, Dept. of Mechanical Engineering, National Univ. of Singapore, 3 Engineering Dr. 2, Singapore 117578, Singapore.

2. Associate Professor, Dept. of Mechanical Engineering, National Univ. of Singapore, 9 Engineering Dr. 1, Singapore 117575, Singapore (corresponding author).

3. Senior Research Scientist, Temasek Laboratories, National Univ. of Singapore, 5A Engineering Dr. 1, Singapore 117411, Singapore.

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.1943-5525.0000663

Reference27 articles.

1. Arena A. Lacarbonara W. and Marzocca P. (2011). “Nonlinear aeroelastic formulation for flexible high-aspect ratio wings via geometrically exact approach.” American Institute of Aeronautics and Astronautics Reston VA 4–7.

2. Atreya S. Mata M. Jones R. and Kohout L. (2005). “Power system comparisons for a high altitude long endurance (HALE) remotely operated aircraft (ROA).” AIAA 5th Aviation Technology Integration and Operations Conf. (ATIO) American Institute of Aeronautics and Astronautics Reston VA.

3. Flight Dynamics of Highly Flexible Aircraft

4. Colozza A. (2003). “Initial feasibility assessment of a high altitude long endurance airship.” NASA/CR 2003-212724.

5. Foch R. J. and Ailinger K. G. (1992). “Low Reynolds number long endurance aircraft design.” American Institute of Aeronautics and Astronautics Reston VA.

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