A. Seginer

发表

Magnus effects at high angles of attack and critical Reynolds numbers

A. Seginer, M. Ringel, 1986 .

Aerodynamics of wraparound fins

A. Seginer, B. Bar-Haim, 1983 .

Performance augmentation of a 60-degree delta aircraft configurationby spanwise blowing

M. Salomon, A. Seginer, A. Seginer, 1986 .

Propagation of small‐amplitude displacement waves on a vortex in the center of a circular tube

Zvi Rusak, A. Seginer, 1993 .

Pulsating spanwise blowing on a fighter aircraft

A. Seginer, J. Meyer, A. Seginer, 1992 .

A non-integral, axial-force measuring element

D. Levin, A. Seginer, M. Ringel, 1989 .

Augmentation of Fighter-Aircraft Performance by Spanwise Blowing over the Wing Leading Edge

M. Salomon, A. Seginer, A. Seginer, 1983 .

Vortex trajectories and breakdown on wing-canard configurations

A. Seginer, A. Seginer, J. Er-El, 1985 .

Convergence characteristics of a vortex-lattice method for nonlinear configuration aerodynamics

Zvi Rusak, E. Wasserstrom, A. Seginer, 1985 .

Effects of Periodic Spanwise Blowing on Delta-Wing Configuration Characteristics

A. Seginer, A. Seginer, J. Meyer, 1994 .