Robust Aeroelastic Design Optimization of Hypersonic Wings Considering Uncertainty in Heat Flux
Author:
Affiliation:
1. School of Aeronautic Science and Engineering, Beihang University
Publisher
Japan Society for Aeronautical and Space Sciences
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://www.jstage.jst.go.jp/article/tjsass/60/3/60_T-16-23/_pdf
Reference28 articles.
1. 1) McNamara, J. J., Friedmann, P. P., Powell, K., Thuruthimattam, B., and Bartels, R.: Aeroelastic and Aerothermoelastic Behavior in Hypersonic Flow, AIAA J., 46 (2008), pp. 2591–2610.
2. 2) Wan, Z. Q., Wang, Y. K., Liu, Y. Z., and Yang, C.: A High-efficiency Aerothermoelastic Analysis Method, Sci. China-Phys. Mech. Astron., 57 (2014), pp. 1111–1118.
3. 3) Dugundji, J. and Calligeros, J. M.: Similarity Laws for Aerothermoelastic Testing, J. Aerosp. Sci., 29 (1962), pp. 935–950.
4. 4) Dai, Y. T. and Yang, C.: Methods and Advances in the Study of Aeroelasticity with Uncertainties, Chin. J. Aeronaut., 27 (2014), pp. 461–474.
5. 5) Hosder, S., Walters, R. W., and Balch, M.: Efficient Uncertainty Quantification Applied to the Aeroelastic Analysis of a Transonic Wing, AIAA Paper 2008-729, 2008.
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