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10 items by relevance
1 Book chapter

A Study of Hybrid Airfoil Design Method

Zhu, Dong, Yu; Yu, Lei; Yang, Long

Proceedings of the 2018 Asia-pacific International Symposium on Aerospace Technology (apisat 2018) — 2019, Volume 459, pp. 3-18

and a shorter aft section. The aft section is usually designed to provide full scale flow field and droplet impingement on the leading edge. A newly developed method is to design the aft section to provide full scale airfoil surface pressure coefficient. This paper examined the “same surface pressure

Year: 2019

Language: English

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2 Preprint article

An inverse method with regularity condition for transonic airfoil design

Wu, Liyi; Zhu, Ziqiang; Xia, Zhixun

distribution. The same constraint exists at compressible speeds. Presented here is an inverse design method for transonic airfoils. In this method, the target pressure distribution contains a free parameter that is adjusted during the computation to satisfy the regularity condition. Some design results

Year: 1991

Language: Undetermined

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3 Journal article

An inverse method with regularity condition for transonic airfoil design

Wu, L., Y.; Zhu, Z., Q.; Xia, Z., X.

Acta Mechanica — 1992, Volume 95, Issue 1, pp. 59-68

) on the prescribed pressure distribution. The same constraint exists at compressible speeds. In this paper, an inverse design method for transonic airfoil is presented. In the method, the target pressure distribution contains a free parameter that is adjusted during the computation to satisfy the regularity

Year: 1992

Language: English

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4 Journal article

Integrated airfoil and blade design method for large wind turbines

Zhu, Wei Jun; Shen, Wen Zhong; Sørensen, Jens Nørkær

Renewable Energy — 2014, Volume 70, pp. 172-183

This paper presents an integrated method for designing airfoil families of large wind turbine blades. For a given rotor diameter and a tip speed ratio, optimal airfoils are designed based on the local speed ratios. To achieve a high power performance at low cost, the airfoils are designed

Year: 2014

Language: English

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5 Conference paper

Integrated airfoil and blade design method for large wind turbines

Zhu, Wei Jun; Shen, Wen Zhong

Proceedings of the 2013 International Conference on Aerodynamics of Offshore Wind Energy Systems and Wakes (icowes2013) — 2013

This paper presents an integrated method for designing airfoil families of large wind turbine blades. For a given rotor diameter and tip speed ratio, the optimal airfoils are designed based on the local speed ratios. To achieve high power performance at low cost, the airfoils are designed

Year: 2013

Language: English

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6 Conference paper

Application of Improved CST Method in Airfoil Design of Flying Robot

Zhu, Zhe; Guo, Hongwu

2019 Ieee 3rd Advanced Information Management, Communicates, Electronic and Automation Control Conference (imcec) — 2019, pp. 145-149

The following topics are dealt with: feature extraction; power engineering computing; mobile robots; control system synthesis; neural nets; three-term control; learning (artificial intelligence); power grids; object detection; fault diagnosis.

Year: 2019

Language: English

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7 Journal article

An experience-independent inverse design optimization method of compressor cascade airfoil

Zhu, Yujie; Ju, Yaping; Zhang, Chuhua

Proceedings of the Institution of Mechanical Engineers, Part A: Journal of Power and Energy — 2019, Volume 233, Issue 4, pp. 431-442

Year: 2019

Language: English

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8 Journal article

Comparison of two design methods of aerodynamic biobjectives for airfoil and wing shapes

Zhu, Ziqiang; Fu, Hongyan; Liu, Hang; Wang, Xiaolu

Science in China Series E: Technological Sciences — 2004, Volume 47, Issue 2, pp. 203-215

of a flap is determined through optimization using a deterministic method. In supersonic flight the flaps are not deflected due to the requirement of having a minimum drag. For comparison the aerodynamic characteristics of a BO airfoil and wing is calculated. A parallel genetic algorithm is used in BO

Year: 2004

Language: English

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9 Journal article

Proper orthogonal decomposition assisted inverse design optimisation method for the compressor cascade airfoil

Zhu, Yujie; Ju, Yaping; Zhang, Chuhua

Aerospace Science and Technology — 2020, Volume 105, pp. 105955

Inverse design is by far the most physically explicit method in the turbomachinery field for designing a cascade airfoil shape for a prescribed distribution of aerodynamic parameters on the airfoil surface. However, a vital drawback of the available inverse design methods for cascade airfoils

Year: 2020

Language: English

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