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  1. 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
  2. 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
  3. 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
  4. 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
  5. The article represents the discussion of several separate directions of investigations, which are performed by TsAGI flight vehicles aerodynamics specialists at the time. There are some major trends of classic...

    Authors: Sergey L. Chernyshev, Sergey V. Lyapunov and Andrey V. Wolkov
    Citation: Advances in Aerodynamics 2019 1:7
  6. How to solve the hypersonic aerothermodynamics around large-scale uncontrolled spacecraft during falling disintegrated process from outer space to earth, is the key to resolve the problems of the uncontrolled ...

    Authors: Zhi-Hui Li, Ao-Ping Peng, Qiang Ma, Lei-Ning Dang, Xiao-Wei Tang and Xue-Zhou Sun
    Citation: Advances in Aerodynamics 2019 1:4
  7. An array of subsonic counter-flow jets is studied as an active thermal protection system (TPS) for wing leading edges of hypersonic vehicles. The performance is numerically estimated in the model case of a cir...

    Authors: Taku Ohwada, Tomonori Shimada and Takuma Kato
    Citation: Advances in Aerodynamics 2019 1:1

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Annual Journal Metrics

  • 2022 Citation Impact
    2.3 - 2-year Impact Factor
    2.3 - 5-year Impact Factor
    1.092 - SNIP (Source Normalized Impact per Paper)
    0.598 - SJR (SCImago Journal Rank)

    2023 Speed
    8 days submission to first editorial decision for all manuscripts (Median)
    85 days submission to accept (Median)

    2023 Usage 
    257,747 downloads
    13 Altmetric mentions