TY - JOUR
T1 - Linear unsteady CFD of vibrating blades of turbomachinery
AU - Ishida, H.
AU - Yamasaki, N.
AU - Aotsuka, M.
PY - 2013
Y1 - 2013
N2 - This paper presents the numerical calculation of unsteady aerodynamic forces on the vibrating cascade blade row using the implicit time integration method. It is confirmed that first and second-order Euler methods, which are the implicit methods, require less computational time than the third-order Runge-Kutta method, which is the explicit method, by two orders of magnitude.
AB - This paper presents the numerical calculation of unsteady aerodynamic forces on the vibrating cascade blade row using the implicit time integration method. It is confirmed that first and second-order Euler methods, which are the implicit methods, require less computational time than the third-order Runge-Kutta method, which is the explicit method, by two orders of magnitude.
UR - http://www.scopus.com/inward/record.url?scp=84893352876&partnerID=8YFLogxK
UR - http://www.scopus.com/inward/citedby.url?scp=84893352876&partnerID=8YFLogxK
U2 - 10.1016/j.proeng.2013.12.019
DO - 10.1016/j.proeng.2013.12.019
M3 - Conference article
AN - SCOPUS:84893352876
SN - 1877-7058
VL - 67
SP - 197
EP - 206
JO - Procedia Engineering
JF - Procedia Engineering
T2 - 7th Asian-Pacific Conference on Aerospace Technology and Science, APCATS 2013
Y2 - 23 May 2013 through 26 May 2013
ER -