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Effect of Various Boundary Conditions on the Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile
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$a Effect of Various Boundary Conditions on the Supersonic Flow Through the Tip-Section Turbine Blade Cascade with a Flat Profile 215 $a 2 s. $c P 463 -1
$1 001 cav_un_epca*0510718 $1 010 $a 978-80-261-0889-4 $1 200 1 $a Proceedings of Computational mechanics 2019 $v S. 133-134 $1 210 $a Plzeň $c University of West Bohemia $d 2019 $1 702 1 $4 340 $a Adámek $b V. $1 702 1 $4 340 $a Jonášová $b A. $1 702 1 $4 340 $a Plánička $b S. $1 702 1 $4 340 $a Zajíček $b M. 610 $a turbine cascade 610 $a transition model 610 $a shock wave-boundary layer interaction 700 -1
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$3 cav_un_auth*0101943 $4 070 $a Příhoda $b Jaromír $p UT-L $i D 1 - Dynamika tekutin $j D 1 - Fluid Dynamics $w D1 – Fluid Dynamics $y CZ $T Ústav termomechaniky AV ČR, v. v. i. 701 -1
$3 cav_un_auth*0096448 $4 070 $a Fürst $b J. $y CZ 856 $q PDF
Number of the records: 1