H. Försching

发表

Flutter Stability of the Annular Wing in Incompressible Flow.

H. Försching, K. v.Diest, 1990 .

A Parametric Study of the Aeroelastic Stability of a Binary Wing-with-engine Nacelle Flutter System in Incompressible Flow.

H. Försching, A. Senft, 1991 .

Parametric Studies of the Flutter Stability Characteristics of Turbomachine Bladings

H. Försching, 1998 .

Parametric Study of the Flutter Stability of a Swept-Back Half-Wing with Engine Nacelle in Subsonic Flow.

H. Försching, C. Keßler, 1994 .

The Expanding Domain of Aeroelastic Simulation.

H. Hönlinger, H. Försching, 1996 .

The Impact of Aeroelasticity on the design of New Ultra High Capacity Aircraft (UHCA).

H. Försching, 1993 .

A Parametric Study of the Flutter Stability Characteristics of Turbomachine Cascades.

H. Försching, 1996 .

Challenges and Perspectives in Computational Aeroelasticity.

H. Försching, H. Försching, 1995 .

Aeroelastic stability of cascades in turbomachinery

H. Försching, H. Försching, 1994 .

New ultra high capacity aircraft (UHCA) ― challenges and problems from an aeroelastic point of view

H. Försching, H. Försching, 1994 .

Structures and Materials in the 90s - Concept and Prospects.

H. Försching, 1990 .

Unsteady Aerodynamic Forces on an Oscillating Wing at High Incidences and Flow Separation.

H. Försching, 1990 .

Flutter stability of annular wings in incompressible flow

H. Försching, K. von Diest, 1991 .

A parametric study of the flutter stability of two-dimensional turbine and compressor cascades in incompressible flow

H. Försching, H. Försching, 1989 .