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Flutter methodology using reduced order aeroelastic model
SYS 0549611 LBL 01000a^^22220027750^450 005 20231122150204.5 017 $2 DOI 100 $a 20211214d m y slo 03 ba 101 $a eng $d eng 102 $a CZ 200 1-
$a Flutter methodology using reduced order aeroelastic model 210 $a Praha $c Ústav termomechaniky AV ČR, v. v. i. $d 2021 215 $a 24 s. $c P 610 $a reduced order model (ROM) 610 $a classical flutter 610 $a steam turbine blade 610 $a panel 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*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. 701 -1
$3 cav_un_auth*0366788 $a Šnábl $b Pavel $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.
Počet záznamů: 1