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A computational methodology for a micro launcher engine tes..:
Ion DIMA
;
Adrian TOADER
;
Dragos Daniel ION GUTA
.
http://bulletin.incas.ro/files/dima__toader__ion-guta__bocioaga__vol_9_iss_1.pdf. , 2017
Link:
https://doi.org/10.13111/2066-8201.2017.9.1.3
RT Journal T1
A computational methodology for a micro launcher engine test bench using a combined linear static and dynamic in frequency response analysis
UL https://suche.suub.uni-bremen.de/peid=base-ftdoajarticles:oai:doaj.org_article:6000e20f0c684315aff795ba327f3cca&Exemplar=1&LAN=DE A1 Ion DIMA A1 Adrian TOADER A1 Dragos Daniel ION GUTA A1 Mircea BOCIOAGA PB National Institute for Aerospace Research "Elie Carafoli" - INCAS YR 2017 K1 Implicit Nonlinear K1 Frequency Response K1 Linear Static K1 NASTRAN K1 Krylov K1 PATRAN K1 PARAM K1 DFREQ K1 von Mises Stress K1 bdf file K1 OP2 file K1 combined static and dynamic analysis K1 Motor vehicles. Aeronautics. Astronautics K1 TL1-4050 JF http://bulletin.incas.ro/files/dima__toader__ion-guta__bocioaga__vol_9_iss_1.pdf LK http://dx.doi.org/https://doi.org/10.13111/2066-8201.2017.9.1.3 DO https://doi.org/10.13111/2066-8201.2017.9.1.3 SF ELIB - SuUB Bremen
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