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Advances in Aerodynamics
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  2. The newly developed vortex-identification method, Liutex, has provided a new systematic description of the local fluid rotation, which includes scalar, vector, and tensor forms. However, the advantages of Liut...

    Authors: Pushpa Shrestha, Charles Nottage, Yifei Yu, Oscar Alvarez and Chaoqun Liu

    Citation: Advances in Aerodynamics 2021 3:8

    Content type: Research

    Published on:

  6. In this era of fast-depleting natural resources, the hike in fuel prices is ever-growing. With stringent norms over environmental policies, the automotive manufacturers are on a voyage to produce efficient veh...

    Authors: Devang S. Nath, Prashant Chandra Pujari, Amit Jain and Vikas Rastogi

    Citation: Advances in Aerodynamics 2021 3:4

    Content type: Research

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  7. With the increasing of computing ability, large-scale simulations have been generating massive amounts of data in aerodynamics. Sort-last parallel rendering is the most classical image compositing method for l...

    Authors: Min Hou, Chongke Bi, Fang Wang, Liang Deng, Gang Zheng and Xiangfei Meng

    Citation: Advances in Aerodynamics 2021 3:3

    Content type: Research

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  8. The effectiveness of the Vectored Thrust Ducted Propeller (VTDP) system is not high currently, especially the lateral force is not large enough. Thus, a conceptual design for a deflection device of a VTDP syst...

    Authors: Yongwei Gao, Jianming Zhang, Long Wang, Bingzhen Chen and Binbin Wei

    Citation: Advances in Aerodynamics 2021 3:2

    Content type: Research

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  10. Properties of wall pressure beneath a transitional hypersonic boundary layer over a 7∘ half-angle blunt cone at angle of attack 6∘ are studied by Direct Numerical Simulation. The wall pressure has two distinct fr...

    Authors: Siwei Dong, Jianqiang Chen, Xianxu Yuan, Xi Chen and Guoliang Xu

    Citation: Advances in Aerodynamics 2020 2:29

    Content type: Research

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  11. The evacuated tube transportation has great potential in the future because of its advantages of energy saving and environmental protection. The train runs in the closed tube at ultra-high speed. The heat quan...

    Authors: Shijie Bao, Xiao Hu, Jukun Wang, Tianhao Ma, Yingyu Rao and Zigang Deng

    Citation: Advances in Aerodynamics 2020 2:28

    Content type: Research

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  12. The computation of compressible flows at all Mach numbers is a very challenging problem. An efficient numerical method for solving this problem needs to have shock-capturing capability in the high Mach number ...

    Authors: Yanqun Jiang, Xun Chen, Xu Zhang, Tao Xiong and Shuguang Zhou

    Citation: Advances in Aerodynamics 2020 2:27

    Content type: Research

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  13. In this paper, we introduce the discrete Maxwellian equilibrium distribution function for incompressible flow and force term into the two-stage third-order Discrete Unified Gas-Kinetic Scheme (DUGKS) for simul...

    Authors: Rui Zhang, Chengwen Zhong, Sha Liu and Congshan Zhuo

    Citation: Advances in Aerodynamics 2020 2:26

    Content type: Research

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  14. Accuracy of unstructured finite volume discretization is greatly influenced by the gradient reconstruction. For the commonly used k-exact reconstruction method, the cell centroid is always chosen as the reference...

    Authors: Lingfa Kong, Yidao Dong, Wei Liu and Huaibao Zhang

    Citation: Advances in Aerodynamics 2020 2:25

    Content type: Research

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  20. Nearly all illuminating classic hypersonic flow theories address aerodynamic phenomena as a perfect gas in the high-speed range and at the upper limit of continuum gas domain. The hypersonic flow is quantitati...

    Authors: Joseph J. S. Shang and Hong Yan

    Citation: Advances in Aerodynamics 2020 2:19

    Content type: Review

    Published on:

    The Correction to this article has been published in Advances in Aerodynamics 2020 2:22

  21. Since the classical weighted essentially non-oscillatory (WENO) scheme is proposed, various improved versions have been developed, and a typical one is the WENO-Z scheme. Although better resolution is achieved...

    Authors: Zheng Hong, Zhengyin Ye and Kun Ye

    Citation: Advances in Aerodynamics 2020 2:18

    Content type: Research

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  22. In this paper, we present a hybrid grid generation approach for viscous flow simulations by marching a surface triangulation on viscous walls along certain directions. Focuses are on the computing strategies u...

    Authors: Hongfei Ye, Yang Liu, Bo Chen, Zhiwei Liu, Jianjing Zheng, Yufei Pang and Jianjun Chen

    Citation: Advances in Aerodynamics 2020 2:17

    Content type: Research

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  26. A truly three-dimensional (3D) gas-kinetic flux solver for simulation of incompressible and compressible viscous flows is presented in this work. By local reconstruction of continuous Boltzmann equation, the i...

    Authors: Y. Sun, L. M. Yang, C. Shu and C. J. Teo

    Citation: Advances in Aerodynamics 2020 2:13

    Content type: Research

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  27. The flow of an active thermal protection system exploiting subsonic counter-flow jets for wing leading edges of hypersonic vehicles is numerically studied on the basis of the three dimensional Navier-Stokes eq...

    Authors: Tomonori Shimada and Taku Ohwada

    Citation: Advances in Aerodynamics 2020 2:12

    Content type: Research

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  30. The unsteady transonic aerodynamics of a wing-body configuration is investigated by solving the Unsteady Reynolds-averaged Navier-Stokes equations closed with the full Reynolds Stress Model. This work presents...

    Authors: Razvan Marian Apetrei, Vlad Ciobaca, Jose Luis Curiel-Sosa and Ning Qin

    Citation: Advances in Aerodynamics 2020 2:9

    Content type: Research

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  31. Blunt-body configurations are the most common geometries adopted for non-lifting re-entry vehicles. Hypersonic re-entry vehicles experience different flow regimes during flight due to drastic changes in atmosp...

    Authors: T. Chourushi, A. Rahimi, S. Singh and R. S. Myong

    Citation: Advances in Aerodynamics 2020 2:8

    Content type: Research

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  32. The DSMC modeling is developed to simulate three-dimensional (3D) rarefied ionization flows and numerically forecast the communication blackout around spacecraft during hypervelocity reentry. A new weighting f...

    Authors: Ming Fang, Zhi-Hui Li, Zhong-Hua Li, Jie Liang and Yong-Hao Zhang

    Citation: Advances in Aerodynamics 2020 2:7

    Content type: Research

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  34. Recently, a novel concept of flapping Micro-Air-Vehicles (FMAVs) with four wings has been proposed, which potentially utilizes the clap-and-fling effect for lift enhancement and agile maneuvers through an adju...

    Authors: Cheng Cheng, Jianghao Wu, Yanlai Zhang, Han Li and Chao Zhou

    Citation: Advances in Aerodynamics 2020 2:5

    Content type: Research

    Published on:

    The Correction to this article has been published in Advances in Aerodynamics 2020 2:16

  35. Despite over fifty years of research on shock wave boundary layer effects and interactions, many related technical issues continue to be controversial and debated. The present survey provides an overview of th...

    Authors: P. M. Ligrani, E. S. McNabb, H. Collopy, M. Anderson and S. M. Marko

    Citation: Advances in Aerodynamics 2020 2:4

    Content type: Review

    Published on:

  40. A three-dimensional-membrane-type wing is investigated applying fluid-structure-interaction computations and complementary experiments. An analysis for three Reynolds numbers is conducted at various angles of ...

    Authors: J. Piquee, I. López Canalejo, C. Breitsamter, R. Wüchner and K.-U. Bletzinger

    Citation: Advances in Aerodynamics 2019 1:20

    Content type: Research

    Published on:

  42. The accuracy of gradient reconstruction methods on unstructured meshes is analyzed both mathematically and numerically. Mathematical derivations reveal that, for gradient reconstruction based on the Green-Gaus...

    Authors: Nianhua Wang, Ming Li, Rong Ma and Laiping Zhang

    Citation: Advances in Aerodynamics 2019 1:18

    Content type: Research

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  45. For the general case of a spatial isoenergetic flow of ideal gas, Helmholtz’s theorems are generalized and the speed with which vortex tubes move is found, keeping the intensity. It is shown that along the str...

    Authors: V. N. Golubkin and G. B. Sizykh

    Citation: Advances in Aerodynamics 2019 1:15

    Content type: Research

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  46. The paper presents the experimental results and the results of direct numerical simulation of the development and interaction of two wave trains from two point sources of controlled disturbances in a supersoni...

    Authors: G. L. Kolosov, A. D. Kosinov, A. N. Semenov and A. A. Yatskikh

    Citation: Advances in Aerodynamics 2019 1:14

    Content type: Research

    Published on:

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  • Advances in Aerodynamics is affiliated with the Chinese Aerodynamics Research Society, which is supported by China Aerodynamics Research and Development Center. 

    Chinese Aerodynamics Research Society (CARS) is a national, academic and non-profit social organization voluntarily formed by the academics practitioners and institutions engaged in aerodynamic research. It is also a constituent of China Association for Science and Technology.

    Dedicated to promoting academic exchanges and scientific popularization in the field of aerodynamics in China, CARS has published several professional journals and organized activities such as Chinese Conference of Aerodynamics Annual Meeting, National Aeroelastic Academic Exchange Meeting, National Conference on Computational Fluid Dynamics.

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  • ISSN: 2524-6992 (electronic)
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