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Analysis of nonstationary separation flow around a thin profile

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Literature Cited

  1. E. Wedemeyer, “Ausbildung eines Wirbelpaares an den Kanten einer Platte,” Ingr-Arch.,30, No. 3 (1961).

  2. N. D. Ham, “Aerodynamic loading on a two-dimensional airfoil during dynamic stall,” AIAA J., No. 10 (1968).

  3. R. H. Djojodihardjo and S. E. Widnall, “A numerical method for the calculation of nonlinear unsteady lifting potential flow problems,” AIAA J., No. 10 (1969).

  4. S. M. Belotserkovskii, “Computation of the flow around wings of arbitrary planform in a broad range of angles of attack,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 4 (1968).

  5. S. M. Belotserkovskii, “Method of computing the effect of separation on an arbitrary thin wing,” Izv. Akad. Nauk SSSR, Mekhan. Zhidk. i Gaza, No. 1 (1966).

  6. G. K. Batchelor, An Introduction to Fluid Dynamics, Cambridge University Press (1967).

  7. S. M. Gorlin and G. E. Khudyakov, “Influence of initial stream turbulence on the aerodynamic characteristics of a flat plate,” Institute of Mechanics, Moscow State University, Scientific Paper No. 4 (1970).

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Moscow. Translated from Izvestya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 3, pp. 177–182, May–June, 1972.

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Belotserkovskii, S.M., Nisht, M.I. Analysis of nonstationary separation flow around a thin profile. Fluid Dyn 7, 525–529 (1972). https://doi.org/10.1007/BF01209061

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  • DOI: https://doi.org/10.1007/BF01209061

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