Calculation of the laminar boundary layer in a compressible gas in the presence of suction or blowing
Lju Šèn'-cjuan'

This publication is cited in the following articles:

1. K. G. Garaev, I. R. Mukhametzyanov, “Optimally controlled turbulent boundary layers in supersonic gas flows”, Math. Models Comput. Simul., 15:1 suppl. (2023), S18–S26      
2. G G Bilchenko, N G Bilchenko, “On the influence of linear temperature factor and constant blowing on the values of functionals of hypersonic aerodynamics”, J. Phys.: Conf. Ser., 1479:1 (2020), 012020  
3. G G Bilchenko, N G Bilchenko, “On the influence of linear blowing and constant temperature factor on the values of functionals of hypersonic aerodynamics”, J. Phys.: Conf. Ser., 1479:1 (2020), 012019  
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5. G G Bilchenko, N G Bilchenko, “On two special values of temperature factor in hypersonic flow stagnation point”, J. Phys.: Conf. Ser., 973 (2018), 012027  
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8. Garaev K.G., “Dostatochnye usloviya suschestvovaniya novogo avtomodelnogo resheniya v klassicheskoi teorii laminarnogo pogranichnogo sloya”, Vestnik kazanskogo gosudarstvennogo tekhnicheskogo universiteta im. A.N. Tupoleva, 2011, no. 2, 63–66  
9. Garaev K.G., Kuznetsov V.K., “Ob odnoi invariantnoi variatsionnoi zadache laminarnogo pogranichnogo sloya”, Prikladnaya matematika i mekhanika, 75:4 (2011), 572–580      
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