Literature cited
J. P. Giesing, “Nonlinear two-dimensional unsteady potential flow with lift,∝ J. Aircraft,5, No. 5 (1968).
R. H. Djojodihardjo and S. E. Widnall, “A numerical method for the calculation of nonlinear unsteady lifting potential flow problems,∝ AIAA J.,7, No. 10 (1969).
D. N. Gorelov and R. L. Kulyaev, “Nonlinear problem about the nonstationary incompressible fluid flow around a slender profile,∝ Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 6 (1971).
V. A. Golovkin, “Nonlinear problem about the unsteady flow around an arbitrary profile with a freely deformable vortex wake,∝ Uchen. Zapiski TsAGI,3, No. 3 (1972).
E. Wedemeyer, “Ausbildung eines Wirbelpaares an den Kanten einer Platte,∝ Ingen.-Arch.,30, No. 3 (1961).
N. D. Ham, “Aerodynamic loading on two-dimensional airfoil during dynamic stall,∝ AIAA J.,6, No. 10 (1968).
K. P. Il'ichev and S. N. Postolovskii, “Analysis of the nonstationary separation flow around bodies by a two-dimensional inviscid fluid stream,∝ Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 2 (1972).
S. M. Belotserkovskii and M. I. Nisht, “On the analysis of nonstationary separation flow around a slender profile,∝ Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 3 (1972).
S. M. Belotserkovskii, “Analysis of the flow around wings of arbitrary planform in a broad range of angles of attack,∝ Izv. Akad. Nauk SSSR, Mekhan. Zhidk. Gaza, No. 4 (1968).
S. M. Belotserkovskii, B. K. Skripach, and V. G. Tabachnikov, Wing in a Nonstationary Gas Flow [in Russian], Nauka, Moscow (1971).
S. M. Belotserkovskii, Slender Lifting Surface in a Subsonic Gas Flow [in Russian], Nauka, Moscow (1965).
Author information
Authors and Affiliations
Additional information
Translated from Izvestiya Akademii Nauk SSSR, Mekhanika Zhidkosti i Gaza, No. 4, pp. 100–108, July–August, 1974.
The authors are grateful to O. N. Sokolov for great assistance in realizing the method on a digital computer.
Rights and permissions
About this article
Cite this article
Belotserkovskii, S.M., Nisht, M.I. Nonstationary nonlinear theory of a thin wing of arbitrary planform. Fluid Dyn 9, 583–589 (1974). https://doi.org/10.1007/BF01031317
Received:
Issue Date:
DOI: https://doi.org/10.1007/BF01031317