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Tihao Yang

As seen in: MDPI
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Articles

Aerodynamic Robust Design Research Using Adjoint-Based Optimization under Operating Uncertainties

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By Yuhang Ma, Tihao Yang, Yayun Shi, Jiecheng Du
| MDPI
This is an early access version, the complete PDF, HTML, and XML versions will be available soon. Open AccessArticle by 1, 1, 1,*, 2, 3 and 3 1 School of Aeronautics, Northwestern Polytechnical University, Xi’an 710072, China 2 State Key Laboratory for Strength and Vibration of Mechanical Structures, School of Aerospace Engineering, Xi’an Jiaotong University, Xi’an 710049, China 3 AVIC The First Aircraft Institute, Xi’an 710089, China * Author to whom correspondence should be addressed.
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Adjoint-Based Aerodynamic Design Optimization and Drag Reduction Analysis of a Military Transport Aircraft Afterbody

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By Yifu Chen, Hanyue Rao, Yayun Shi, Tihao Yang
| MDPI
Abstract : Based on the adjoint method, the afterbody of a military transport aircraft was optimized and designed to meet engineering constraints under real flight conditions. Guidance for the key design parameters of the afterbody of the military transport aircraft is given. The vortex dynamics and boundary layer extraction methods were used to analyze the optimization results of military transport aircraft.
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