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Calculation of the flow past plane triangular wings at large angles of attack

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References

  1. G. G. Chernyi, “Wings in hypersonic flow”, PMM, vol. 29, no. 4, 1965.

  2. A. P. Bazzhin, “Calculation of the flow past the lower surface of triangular wings at large angles of attack”, Inzh. zh., vol. 4, no. 2, 1964.

  3. V. V. Sychev, “Three-dimensional hypersonic gas flow past slender bodies at large angles of attack”, PMM, vol. 24, no. 2, 1960.

  4. A. F. Messiter, “Lift of slender delta wings according to Newtonian theory”, JAS Paper no. 62–114.

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  1. Moscow

    A. P. Bazzhin

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  1. A. P. Bazzhin
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Bazzhin, A.P. Calculation of the flow past plane triangular wings at large angles of attack. Fluid Dyn 1, 71–72 (1966). https://doi.org/10.1007/BF01022156

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  • DOI: https://doi.org/10.1007/BF01022156

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