论文信息 - Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle - 字舞流文

Experimental and Numerical Study of the Time-Dependent Pressure Response of a Shock Wave Oscillating in a Nozzle

Keywords: Unsteady Flows ; Numerical Analyses ; Turbomachinery ; GTT ; LTT Reference LTT-CONF-1993-003 Record created on 2007-04-18, modified on 2017-05-10

Torsten Fransson | Peter Ott | A. Bölcs

[1] Peter Ott. Oszillierender senkrechter Verdichtungsstoss in einer ebenen Düse , 1992 .

[2] Sanford Fleeter,et al. Oscillating cascade aerodynamics by an experimental influence coefficient technique , 1990 .

[3] J. M. Verdon. THE UNSTEADY AERODYNAMIC RESPONSE TO ARBITRARY MODES OF BLADE MOTION , 1989 .

[4] Torsten Fransson,et al. Time-Dependent Pressure Fluctuations on an Oscillating Turbine Cascade at Transonic Off-Design Flow Conditions , 1991 .

[5] D. S. Whitehead,et al. A finite element method for the solution of two‐dimensional transonic flows in cascades , 1985 .

[6] S. Liang,et al. Numerical investigation of unsteady transonic nozzle flows , 1992 .

[7] Georg A. Gerolymos. Advances in the Numerical Integration of the 3-D Euler Equations in Vibrating Cascades , 1992 .

[8] James L. Thomas,et al. Extension and applications of flux-vector splitting to unsteady calculations on dynamic meshes , 1987 .

[9] T. C. Adamson,et al. Unsteady motion of shock waves in two dimensional transonic channel flows , 1977 .

[10] Sanford Fleeter,et al. Wind Tunnel Wall Effects in a Linear Oscillating Cascade , 1993 .