Thermal-stress response of hypersonic rudder to laser irradiation

Zhang Li; Wang Gang; Li Mu; Tan Fuli; Zhao Jianheng

doi:10.11884/HPLPB201527.011008

Volume 27 Issue 01

Jan. 2015

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Article Navigation > High Power Laser and Particle Beams > 2015 > 27(01): 011008

Li Wenhuai, Wang Junling, Zhang Xiangju, et al. Optimization of periodical physical flux map test[J]. High Power Laser and Particle Beams, 2017, 29: 016004. doi: 10.11884/HPLPB201729.160199

Citation:

Zhang Li, Wang Gang, Li Mu, et al. Thermal-stress response of hypersonic rudder to laser irradiation[J]. High Power Laser and Particle Beams, 2015, 27: 011008. doi: 10.11884/HPLPB201527.011008

Li Wenhuai, Wang Junling, Zhang Xiangju, et al. Optimization of periodical physical flux map test[J]. High Power Laser and Particle Beams, 2017, 29: 016004. doi: 10.11884/HPLPB201729.160199

Citation:

Zhang Li, Wang Gang, Li Mu, et al. Thermal-stress response of hypersonic rudder to laser irradiation[J]. High Power Laser and Particle Beams, 2015, 27: 011008. doi: 10.11884/HPLPB201527.011008

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Thermal-stress response of hypersonic rudder to laser irradiation

doi: 10.11884/HPLPB201527.011008

1.
Institute of Fluid Physics,CAEP,P.O.Box 919-113,Mianyang 621900,China;
2.
National Key Laboratory of Aerodynamic Design and Research,Northwestern Polytechnical University,Xi’an 710072,China

Received Date: 2014-09-12
Rev Recd Date: 2014-11-20
Publish Date: 2015-01-20

Abstract

Abstract

A static aero elastic model of hypersonic aircraft under laser irradiation was built based on computational fluid dynamics (CFD) and computational structural dynamics coupling numerical computational methodology. The flow was governed by 3-D Reynolds averaged Navier-Stokes equations. To split the viscosity flux and the convective flux of the NS equations, the second order central scheme and the AUSM+up scheme were adopted respectively. With the implicit Gauss-Seidel scheme, the code was advanced in time. The Menter SST turbulence model was used for turbulence simulations. The model was proofread with the experiment data from von Karman Institute hypersonic wind tunnel. Hypersonic aircraft wing under laser irradiation was simulated with this model. The results indicated that the energy addition could reduce the Youngs modulus of hypersonic rudder. Hypersonic aircraft may prang due to the destroy of the rudder.
- laser irradiation,
- hypersonic rudder,
- thermal-stress analysis,
- numerical simulation

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