Agard Manual On Aeroelasticity In Axial Flow Turbomachines V 2 Structural Dynamics And Aeroelasticity

AGARD Manual on Aeroelasticity in Axial-Flow Turbomachines - V.2 - Structural Dynamics and Aeroelasticity

Unsteady Aerodynamics and Aeroelasticity of Turbomachines

Twenty-one years have passed since the first symposium in this series was held in Paris (1976). Since then there have been meetings in Lausanne (1980), Cambridge (1984), Aachen (1987), Beijing (1989), Notre Dame (1991) and Fukuoka (1994). During this period a tremendous development in the field of unsteady aerodynamics and aeroelasticity in turbomachines has taken place. As steady-state flow conditions become better known, and as blades in the turbomachine are constantly pushed towards lower weight, and higher load and efficiency, the importance of unsteady phenomena appear more clearly. th The 8 Symposium was, as the previous ones, of high quality. Furthermore, it presented the audience with the latest developments in experimental, numerical and theoretical research. More papers than ever before were submitted to the conference. As the organising committee wanted to preserve the uniqueness of the symposium by having single sessions, and thus mingle speakers and audience with different backgrounds in this interdisciplinary field, only a limited number of papers could be accepted. 54 papers were accepted and presented at the meeting, all of which are included in the present proceedings.

AGARD Manual on Aeroelasticity in Axial-flow Turbomachines. Vol.2: Structural Dynamics and Aeroelasticity (Advisory Group for Aerospace Research and Development).