Experimental-numerical investigation of the dynamic stability of flexural-torsional vibrations of compressor blades under conditions of attached and separated flow. Part 1. Procedure and equipment for the determination of nonstationary aerodynamic charact

A. L. Stel’makh، نويسنده , , A. D. Len and A. P. Zinkovskii ، نويسنده ,

روزنامه با شماره پیاپی سال 2007

11

200

210

compressor - blades - flat-plate airfoil cascade - flexural-torsional vibrations - nonstationary aerodynamic characteristics - aerodynamic stability

Strength of Materials

2007

Strength of Materials

343952