Technical Papers
Nov 29, 2017

Conceptual Design of Stratospheric Airships Focusing on Energy Balance

Publication: Journal of Aerospace Engineering
Volume 31, Issue 2

Abstract

Stratospheric airships can perform long-duration, wide-area observation missions above a specific location. The conceptual design of streamlined stratospheric airships is researched in this paper. Multidisciplinary analysis models for stratospheric airships are established, including geometry, aerodynamics, propulsion, and renewable power systems. A conceptual design method focusing on the energy balance for stratospheric airships is proposed, taking minimum total mass as the objective function. A conceptual design of a stratospheric airship for area observation was achieved, and the feasibility of the design results was verified. In addition, the influence of the wind resistance strategy on the conceptual design was analyzed, and simulation results showed that, by adjusting power consumption during day and night with a maneuverable wind resistance strategy, the total mass and renewable power system mass of the stratospheric airship can be greatly reduced.

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References

Alam, M. I., and Pant, R. S. (2013). “A methodology for conceptual design and optimization of a high altitude airship.” AIAA Lighter-Than-Air Systems Technology Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–8.
Androulakakis, S. P., and Judy, R. A. (2013). “Status and plans of high altitude airship (HAA™) program.” AIAA Lighter-Than-Air Systems Technology Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–9.
Belmont, A. D., Dartt, D. G., and Nastrom, G. D. (1975). “Variations of stratospheric zonal winds, 20–65 km, 1961–1971.” J. Appl. Meteorol., 14(4), 585–594.
Bents, D. J. (2011). “Long-duration low- to medium-altitude solar electric airship concept.”, National Aeronautics and Space Administration, Washington, DC.
Ceruti, A., Voloshin, V., and Marzocca, P. (2013). “Multi-disciplinary design optimization of unconventional airship configuration using heuristic algorithm.” 54th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–20.
Colozza, A. (2003). “Initial feasibility assessment of a high altitude long endurance airship.”, National Aeronautics and Space Administration, Washington, DC.
Farley, R. E. (2005). “BalloonAscent: 3-D simulation tool for the ascent and float of high-altitude balloons.” AIAA Aviation, Technology Integration and Operations Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–15.
Haque, A. U., Asrar, W., Omar, A. A., Sulaeman, E., and Ali, M. J. S. (2014). “Conceptual design of a winged hybrid airship.” AIAA Lighter-Than-Air Systems Technology Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–24.
Harada, K. (2005). “Ground-to-stratosphere flight test report-ascent simulation of the test vehicle.”, Japan Aerospace Exploration Agency, Tokyo.
Jui, S. H. (1986). Solar energy engineering, Prentice-Hall, Upper Saddle River, NJ.
Kalnay, E., Knanmitsu, M., Kistler, R., Collins, W., and Deaven, D. (1996). “The NCEP/NCAR 40-year reanalysis project.” Bull. Am. Meteorol. Soc., 77(3), 437–471.
Khoury, G. A., and Gillett, J. A. (1999). Airship technology, Cambridge University Press, Cambridge, U.K.
Liang, H. Q., Zhu, M., and Guo, X. (2012). “Conceptual design optimization of a high altitude airship in concurrent subspace optimization.” AIAA Aerospace Sciences Meeting, American Institute of Aeronautics and Astronautics, Reston, VA, 1–17.
Lobbia, M. A., and Gong, R. H. (2006). “A modular sizing model for high-altitude/long-endurance airships.” 44th AIAA Aerospace Sciences Meeting and Exhibit, American Institute of Aeronautics and Astronautics, Reston, VA, 1–9.
Lutz, T., and Wagner, S. (1998). “Drag reduction and shape optimization of airship bodies.” J. Aircr., 35(3), 345–351.
Nejati, V., and Matsuuchi, K. (2003). “Aerodynamics design and genetic algorithms for optimization of airship bodies.” Bull. JSME, 46(4), 610–617.
Oliveira, F. A., Lourenco, F. C., and Devezas, T. C. (2016). “High-altitude platforms—Present situation and technology trends.” J. Aerosp. Technol. Manage., 8(3), 249–262.
Ozoroski, T. A., Mas, K. G., and Hahn, A. S. (2003). “A PC-based design and analysis system for lighter-than-air unmanned vehicles.” AIAA “Unmanned Unlimited” Systems, Technologies, and Operations, American Institute of Aeronautics and Astronautics, Reston, VA, 1–15.
Palumbo, R., Russo, M., and Filippone, E. (2007). “ACHAB: Analysis code for high-altitude balloons.” AIAA Atmospheric Flight Mechanics Conf. and Exhibit, American Institute of Aeronautics and Astronautics, Reston, VA, 1–11.
Pant, R. S. (2008). “Methodology for determination of baseline specifications of a nonrigid airship.” J. Aircr., 45(6), 2177–2182.
Ren, G. Y., Zhang, A. Y., Wang, Y., and Guo, J. (2009). “Climatology of upper wind speeds over China.” Geograph. Res., 28(6), 1583–1592 (in Chinese).
Roney, J. A. (2007). “Statistical wind analysis for near-space applications.” J. Atmos. Sol. Terr. Phys., 69(13), 1485–1501.
Smith, S., Lee, M., Fortenberry, M., and Judy, R. (2011). “Hisentinel80: Flight of a high altitude airship.” 11th AIAA Aviation Technology, Integration, and Operations Conf., American Institute of Aeronautics and Astronautics, Reston, VA, 1–14.
Wang, Q. B., Chen, J. A., Fu, G. Y., and Duan, D. P. (2009). “An approach for shape optimization of stratosphere airships based on multidisciplinary design optimization.” J. Zhejiang Univ. Sci. A, 10(11), 1609–1616.
Wang, X. L., and Shan, X. X. (2006). “Shape optimization of stratospheric airship.” J. Aircr., 43(1), 283–286.
Xiao, C. Y., Hu, X., Gong, J. C., and Liu, J. (2008). “Analysis of the characteristics of the stratospheric quasi-zero wind layer over China.” Chin. J. Space Sci., 28(3), 230–235 (in Chinese).
Yang, Y. C., Wang, S., Gu, Y. D., and Li, Y. T. (2012). “Multidisciplinary design optimization of near space airship based on genetic algorithm.” J. Compu. Simul., 29(4), 49–53 (in Chinese).
Zheng, X., and Zhang, A. W. (2013). “Shape optimization of airship based on constrained particle swarm optimization.” J. Inf. Comput. Sci., 10(18), 5849–5857.
Zhou, X. J., Tao, H. B., and Bian, J. C. (2011). “Analysis of the characteristics of zonal wind reverse layer in the lower and middle stratosphere of the Northern Hemisphere and its seasonal variation.” Clim. Env. Res., 16(5), 565–576 (in Chinese).

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Go to Journal of Aerospace Engineering
Journal of Aerospace Engineering
Volume 31Issue 2March 2018

History

Received: Feb 7, 2017
Accepted: Aug 4, 2017
Published online: Nov 29, 2017
Published in print: Mar 1, 2018
Discussion open until: Apr 29, 2018

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Authors

Affiliations

Xixiang Yang [email protected]
Associate Professor, College of Aerospace Science and Engineering, National Univ. of Defense Technology, No. 47, Yanwachi St., Kaifu, Changsha, Hunan Province 410073, China (corresponding author). E-mail: [email protected]
Duoneng Liu, Ph.D.
Lecturer, China Aerodynamics Research and Development Center, No. 6, Second Ring Rd., Mianyang, Sichuan Province 621000, China.

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