CLC number: V27
On-line Access: 2024-08-27
Received: 2023-10-17
Revision Accepted: 2024-05-08
Crosschecked: 2009-09-10
Cited: 9
Clicked: 7647
Quan-bao WANG, Ji-an CHEN, Gong-yi FU, Deng-ping DUAN. An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization[J]. Journal of Zhejiang University Science A, 2009, 10(11): 1609-1616.
@article{title="An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization",
author="Quan-bao WANG, Ji-an CHEN, Gong-yi FU, Deng-ping DUAN",
journal="Journal of Zhejiang University Science A",
volume="10",
number="11",
pages="1609-1616",
year="2009",
publisher="Zhejiang University Press & Springer",
doi="10.1631/jzus.A0820814"
}
%0 Journal Article
%T An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization
%A Quan-bao WANG
%A Ji-an CHEN
%A Gong-yi FU
%A Deng-ping DUAN
%J Journal of Zhejiang University SCIENCE A
%V 10
%N 11
%P 1609-1616
%@ 1673-565X
%D 2009
%I Zhejiang University Press & Springer
%DOI 10.1631/jzus.A0820814
TY - JOUR
T1 - An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization
A1 - Quan-bao WANG
A1 - Ji-an CHEN
A1 - Gong-yi FU
A1 - Deng-ping DUAN
J0 - Journal of Zhejiang University Science A
VL - 10
IS - 11
SP - 1609
EP - 1616
%@ 1673-565X
Y1 - 2009
PB - Zhejiang University Press & Springer
ER -
DOI - 10.1631/jzus.A0820814
Abstract: airship shape is crucial to the design of stratosphere airships. In this paper, multidisciplinary design optimization (MDO) technology is introduced into the design of airship shape. We devise a composite objective function, based on this technology, which takes account of various factors which influence airship performance, including aerodynamics, structures, energy and weight to determine the optimal airship shape. A shape generation algorithm is proposed and appropriate mathematical models are constructed. Simulation results show that the optimized shape gives an improvement in the value of the composite objective function compared with a reference shape.
[1] Banerjee, S., Dutt, N., 2004. Very Fast Simulated Annealing for HW-SW Partitioning. Technical Report CECS-TR-04-17, University of California, Irvine.
[2] Colozza, A., Dolce, J.L., 2005. High-altitude, Long-endurance Airships for Coastal Surveillance. NASAPTM-2005-213427.
[3] Ingber, L., 1993. Adaptive Simulated Annealing (ASA), Global Optimization C-code. Caltech Alumni Association, Pasadena, California. Available from: http://www.ingber.com/#ASA−CODE [Accessed 13/09/08; verified 01/02/09].
[4] Khoury, G.A., Gillett, J.D., 1999. Airship Technology. Cambridge University Press, Cambridge.
[5] Kirkpatrick, S., Gelatt, C.D.Jr., Vecchi, M.P., 1983. Optimization by simulated annealing. Science, 220(4598):671-680.
[6] Lutz, T., Wagner, S., 1998. Drag reduction and shape optimization of airship bodies. Journal of Aircraft, 35(3):345-351.
[7] Metropolis, N., Rosenbluth, A., Rosenbluth, M., Teller, A., Teller, E., 1953. Equation of state calculations by fast computing machines. Journal of Chemical Physics, 21(6):1087-1092.
[8] Natio, H., Eguchi, K., Hoshino, T., Okaya, S., Fujiwara, T., Miwa, S., Nomura, Y., 1999. Design Concept and Analysis of Solar Power Subsystem for SPF Airship Operation. AIAA 99-3913.
[9] Nejati, V., Matsuuchi, K., 2003. Aerodynamics design and genetic algorithms for optimization of airship bodies. JSME International Journal, Series B: Fluids and Thermal Engineering, 46(4):610-617.
[10] Ozoroski, T.A., Mas, K.G., Hahn, A.S., 2003. A PC-based Design and Analysis System for Lighter-than-air Unmanned Vehicles. 2nd AIAA “Unmanned Unlimited” System, Technologies, and Operation-Aerospace, San Diego, California, USA.
[11] Pant, R.S., 2003. A Methodology for Determination of Baseline Specifications of a Non-rigid Airship. AIAA’s 3rd Annual Aviation Technology, Integration, and Operation (ATIO) Technical Forum, Denver, Colorado, USA.
[12] Szu, H., Hartley, R., 1987. Fast simulated annealing. Physics Letters A, 122(3/4):157-162.
[13] Wang, X.L., Shan, X.X., 2006. Shape optimization of stratosphere airship. Journal of Aircraft, 43(1):283-287.
Open peer comments: Debate/Discuss/Question/Opinion
<1>