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Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method
SYS 0535111 LBL 01000a^^22220027750^450 005 20260205163617.9 017 $2 DOI 100 $a 20201126d m y slo 03 ba 101 $a eng $d eng 102 $a GR 200 1-
$a Subsonic stall flutter analysis in 2D blade cascade using hybrid boundary element method 215 $a 11 s. $c P 463 -1
$1 001 cav_un_epca*0537585 $1 010 $a 978-618-85072-0-3 $1 200 1 $a EURODYN 2020 $i Proceedings of the XI International Conference on Structural Dynamics $h 1 $v S. 213-224 $1 210 $a Athens $c National Technical University of Athens (NTUA) $d 2020 $1 702 1 $a Papadrakakis $b M. $4 340 $1 702 1 $a Fragiadakis $b M. $4 340 $1 702 1 $a Papadimitriou $b C. $4 340 610 $a stall flutter 610 $a aeroelasticity 610 $a boundary element method 610 $a discrete vortex particle method 610 $a panel method 610 $a blade cascade 610 $a Viscous-inviscid coupling 700 -1
$3 cav_un_auth*0368412 $a Prasad $b Chandra Shekhar $p UT-L $i D 3 - Dynamika a vibrace $j D 3 - Dynamics and Vibration $w D3 – Dynamics and Vibration $4 070 $T Ústav termomechaniky AV ČR, v. v. i. 701 -1
$3 cav_un_auth*0101931 $a Pešek $b Luděk $p UT-L $i D 3 - Dynamika a vibrace $j D 3 - Dynamics and Vibration $w D3 – Dynamics and Vibration $y CZ $4 070 $T Ústav termomechaniky AV ČR, v. v. i. 856 $q pdf
Počet záznamů: 1