Počet záznamů: 1
Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties
SYS 0563591 LBL 01000a^^22220027750^450 005 20231122150923.0 014 $a 85130095262 $2 SCOPUS 014 $a 000808123300001 $2 WOS 017 $a 10.1016/j.ymssp.2022.109257 $2 DOI 100 $a 20221108d m y slo 03 ba 101 $a eng $d eng 102 $a GB 200 1-
$a Experimental validation of FEM-computed stress to tip deflection ratios of aero-engine compressor blade vibration modes and quantification of associated uncertainties 215 $a 25 s. $c P 463 -1
$1 001 cav_un_epca*0254299 $1 011 $a 0888-3270 $e 1096-1216 $1 200 1 $a Mechanical Systems and Signal Processing $v Roč. 178, October (2022) $1 210 $c Elsevier 610 $a blade tip timing 610 $a FEM validation 610 $a vibration measurements 610 $a blade stresses 700 -1
$3 cav_un_auth*0439824 $a Mohamed $b E.M. $y GB $4 070 701 -1
$3 cav_un_auth*0439825 $a Bonello $b P. $y GB $4 070 701 -1
$3 cav_un_auth*0411112 $a Russhard $b P. $y GB $4 070 701 -1
$3 cav_un_auth*0101938 $a Procházka $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. 701 -1
$3 cav_un_auth*0408587 $a Mekhalfia $b Mohammed Lamine $p UT-L $i D 3 - Dynamika a vibrace $j D 3 - Dynamics and Vibration $y DZ $4 070 $T Ústav termomechaniky AV ČR, v. v. i. 701 -1
$3 cav_un_auth*0392835 $a Tchawou Tchuisseu $b Eder Batista $p UT-L $i D 3 - Dynamika a vibrace $j D 3 - Dynamics and Vibration $y CM $4 070 $T Ústav termomechaniky AV ČR, v. v. i. 856 $u https://www.sciencedirect.com/science/article/pii/S0888327022004058/pdfft?isDTMRedir=true&download=true $9 RIV
Počet záznamů: 1