Alexander D. Kosinov

发表

EXPERIMENTAL INVESTIGATION OF THE SUPERSONIC BOUNDARY LAYER STABILITY ON A SWEPT WING AT MACH NUMBER M = 2

N. V. Semionov, Alexander D. Kosinov, Yu. G. Ermolaev, 2011 .

Constant temperature hot-wire measurements in a short duration supersonic wind tunnel

S. Wagner, Julien Weiss, Helmut Knauss, 2001, The Aeronautical Journal (1968).

EXPERIMENTS ON RELATIVE RECEPTIVITY OF THREE-DIMENSIONAL SUPERSONIC BOUNDARY LAYER TO CONTROLLED DISTURBANCES AND ITS DEVELOPMENT

N. V. Semionov, Alexander D. Kosinov, G. L. Kolosov, 2013 .

A Hybrid Methodology to Evaluate the Effects of Trip Disks on Transonic Wind Tunnel Models

Jeffrey D. Crouch, Kevin Mejia, Alexander D. Kosinov, 2004 .

Experimental Study of Stability and Transition of Supersonic Boundary Layer on Swept Wing at Mach Number 2 - 4

N. V. Semionov, Alexander D. Kosinov, Yu. G. Yermolaev, 2013 .

Experiments on the stability of supersonic laminar boundary layers

A. A. Maslov, Alexander D. Kosinov, A. Maslov, 1990, Journal of Fluid Mechanics.

Experiments on the Nonlinear Instability of Supersonic Boundary Layers

N. V. Semionov, Alexander D. Kosinov, N. Semionov, 1994 .

Experiments on the Artificial Disturbance Evolution in 2D and 3D Spanwise Modulated Boundary Layers at Mach 2 and 2.5

N. V. Semionov, Alexander D. Kosinov, G. L. Kolosov, 2015 .

Experimental Investigation of Separation and Stability of Supersonic Laminar Boundary Layer

Alexander D. Kosinov, S. G. Shevel'kov, 1991 .