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Advances in Aerodynamics
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  3. Three-dimensional particle reconstruction with limited two-dimensional projections is an under-determined inverse problem that the exact solution is often difficult to be obtained. In general, approximate solu...

    Authors: Qi Gao, Shaowu Pan, Hongping Wang, Runjie Wei and Jinjun Wang
    Citation: Advances in Aerodynamics 2021 3:28
    Content type: Research Published on:

    The Correction to this article has been published in Advances in Aerodynamics 2022 4:25

  4. In this work, we extend the characteristic-featured shock wave indicator based on artificial neuron training to 3D high-speed flow simulation on unstructured meshes. The extension is achieved through dimension...

    Authors: Yiwei Feng, Tiegang Liu, Xiaofeng He, Bin Zhang and Kun Wang
    Citation: Advances in Aerodynamics 2021 3:27
    Content type: Research Published on:

  6. Sonic boom reduction has been an urgent need for the development of future supersonic transport, because of the heavy damage of noise pollution. This paper provides a novel concept for supersonic aircraft to r...

    Authors: Liu-qing Ye, Zheng-yin Ye, Kun Ye, Jie Wu and Sheng-jie Miao
    Citation: Advances in Aerodynamics 2021 3:25
    Content type: Research Published on:

  9. Improving resource utilization is an important goal of high-performance computing systems of supercomputing centers. To meet this goal, the job scheduler of high-performance computing systems often uses backfi...

    Authors: Hao Wang, Yi-Qin Dai, Jie Yu and Yong Dong
    Citation: Advances in Aerodynamics 2021 3:22
    Content type: Research Published on:

  11. A newly developed frosting simulation method, p-VOF method, is applied to simulate the dynamic frost formation on the NACA0012 airfoil under strong convection. The p-VOF method is a pseudo VOF method of the mu...

    Authors: Bin Xia, Xianghua Xu and Xingang Liang
    Citation: Advances in Aerodynamics 2021 3:20
    Content type: Research Published on:

  12. This paper presents numerical studies of the Magnus effect for a kinetic turbine on a horizontal axis. To focus on the Magnus blade, a single self-spinning cylindrical blade is assumed. An iterative direct-for...

    Authors: X. Bai, C. Ji, P. Grant, N. Phillips, U. Oza, E. J. Avital and J. J. R. Williams
    Citation: Advances in Aerodynamics 2021 3:19
    Content type: Research Published on:

  13. The unified stochastic particle method based on the Bhatnagar-Gross-Krook model (USP-BGK) has been proposed recently to overcome the low accuracy and efficiency of the traditional stochastic particle methods, ...

    Authors: Fei Fei, Yang Ma, Jie Wu and Jun Zhang
    Citation: Advances in Aerodynamics 2021 3:18
    Content type: Research Published on:

  17. In order to visualize the rarefied flow field in a Φ1m hypersonic low-density wind tunnel, an electric glow discharge technique based on high frequency excited power has been developed. Firstly, finite element...

    Authors: Wanqiu Jiang, Huacheng Qiu, Yanguang Yang, Yilei Shi, Jie Wang, Jie Li, Zhengyi Long and Chunman Mao
    Citation: Advances in Aerodynamics 2021 3:14
    Content type: Research Published on:

  18. The water entry is a classic fluid-structure interaction problem in ocean engineering. The prediction of impact loads on structure during the water entry is critical to some engineering applications. In this p...

    Authors: Zi-Fei Meng, Fu-Ren Ming, Ping-Ping Wang and A-Man Zhang
    Citation: Advances in Aerodynamics 2021 3:13
    Content type: Research Published on:

    The Correction to this article has been published in Advances in Aerodynamics 2021 3:17

  19. In this paper, we present an effective prismatic mesh generation method for viscous flow simulations. To address the prismatic mesh collisions in recessed cavities or slit areas, we exploit 3D tensors controll...

    Authors: Yiming Zhu, Shengfa Wang, Xiaopeng Zheng, Na Lei, Zhongxuan Luo and Bo Chen
    Citation: Advances in Aerodynamics 2021 3:12
    Content type: Research Published on:

  21. A scaled model of the X38-like configuration was simulated under hypersonic conditions for the direct simulation Monte Carlo method and the unified gas kinetic scheme. The inflow conditions considered several ...

    Authors: Jin Li, Dingwu Jiang, Xiangren Geng and Jianqiang Chen
    Citation: Advances in Aerodynamics 2021 3:10
    Content type: Research Published on:

  23. 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:

    The Correction to this article has been published in Advances in Aerodynamics 2021 3:11

  27. 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 Published on:

  28. 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 Published on:

  29. 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 Published on:

  31. 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 Published on:

  32. 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 Published on:

  33. 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 Published on:

  34. 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 Published on:

  35. 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 Published on:

  41. 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

  42. 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 Published on:

  43. 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 Published on:

  47. 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 Published on:

  48. 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 Published on:
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Annual Journal Metrics

  • Citation Impact 2023
    Journal Impact Factor: 2.9
    5-year Journal Impact Factor: 2.9
    Source Normalized Impact per Paper (SNIP): 1.279
    SCImago Journal Rank (SJR): 0.773

    Speed 2023
    Submission to first editorial decision (median days): 8
    Submission to acceptance (median days): 85

    Usage 2023
    Downloads: 257,747
    Altmetric mentions: 13

  • ISSN: 2524-6992 (electronic)
  • ISSN: 2097-3462 (print)