Transonic shock oscillations on NACA0012 aerofoil Export

@article{Raghunathan1998Transonic, abstract = {Abstract.\ \  The mechanism of the origin of shock oscillations on NACA0012 aerofoils is investigated using a moving grid thin layer Navier Stokes code. The method used to understand the mechanism is to initiate the shock oscillations on an aerofoil by moving the aerofoil from a regime of steady transonic flow into a regime of periodic flow by a change in airflow incidence. The results indicate that the shock induced bubble plays a leading role in the origin of shock oscillations and the trailing edge has an affect on its amplitude.}, author = {Raghunathan, S. and Mitchell, R. D. and Gillan, M. A.}, citeulike-article-id = {2132319}, citeulike-linkout-0 = {http://dx.doi.org/10.1007/s001930050113}, day = {10}, doi = {10.1007/s001930050113}, journal = {Shock Waves}, keywords = {buffet, naca0012, navier-stokes, thin-layer}, number = {4}, pages = {191--202}, posted-at = {2007-12-16 13:34:54}, priority = {2}, title = {Transonic shock oscillations on NACA0012 aerofoil}, url = {http://dx.doi.org/10.1007/s001930050113}, volume = {8}, year = {1998} }

TY - JOUR ID - Raghunathan1998Transonic L3 - citeulike-article-id:2132319 N2 - Abstract.   The mechanism of the origin of shock oscillations on NACA0012 aerofoils is investigated using a moving grid thin layer Navier Stokes code. The method used to understand the mechanism is to initiate the shock oscillations on an aerofoil by moving the aerofoil from a regime of steady transonic flow into a regime of periodic flow by a change in airflow incidence. The results indicate that the shock induced bubble plays a leading role in the origin of shock oscillations and the trailing edge has an affect on its amplitude. IS - 4 JF - Shock Waves EP - 202 TI - Transonic shock oscillations on NACA0012 aerofoil VL - 8 SP - 191 KW - buffet KW - naca0012 KW - navier-stokes KW - thin-layer AU - Raghunathan, S AU - Mitchell, RD AU - Gillan, MA PY - 1998//10/ UR - http://dx.doi.org/10.1007/s001930050113 ER -