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Meshfree reduced order model for turbomachinery blade flutter analysis
SYS 0556768 LBL 01000a^^22220027750^450 005 20240111141105.0 014 $a 85127625644 $2 SCOPUS 014 $a 000798733400002 $2 WOS 017 $a 10.1016/j.ijmecsci.2022.107222 $2 DOI 100 $a 20220426d m y slo 03 ba 101 $a eng $d eng 102 $a GB 200 1-
$a Meshfree reduced order model for turbomachinery blade flutter analysis 215 $a 18 s. $c P 463 -1
$1 001 cav_un_epca*0253397 $1 011 $a 0020-7403 $e 1879-2162 $1 200 1 $a International Journal of Mechanical Sciences $v Roč. 222, May (2022) $1 210 $c Elsevier 610 $a aeroelastic instability 610 $a turbomachinery blade flutter 610 $a hybrid 3D panel method 610 $a reduced order aeroelastic model 610 $a boundary element method 610 $a discrete vortex particle method 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*0101896 $a Kolman $b Radek $p UT-L $i D 4 - Rázy a vlny v tělesech $j D 4 - Impact and Waves in Solids $w D4 – Impacts and Waves in Solids and Centre CeNDYNMAT $y CZ $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 dokument $u https://www.sciencedirect.com/science/article/pii/S002074032200145X $9 RIV
Počet záznamů: 1