I. D. Zverkov

Morphine wing as the basis of the aircraft of the future

V. V. Kulikov, A. V. Kryukov, I. D. Zverkov, 2020 .

Creation of subsonic macro-and microjets facilities and automated measuring system (AMS-2) for the spatial – temporal hot – wire anemometric visualization of jet flow field

A. M. Sorokin, I. D. Zverkov, G. R. Grek, 2017 .

Experimental research of the boundary layer structure at near-critical angles of attack for the classical and wavy wings

V. V. Kozlov, I. D. Zverkov, Alexey Kryukov, 2013 .

TRANSITIONAL FLOW STRUCTURE ON CLASSIC AND WAVY WINGS AT LOW REYNOLDS NUMBERS

I. D. Zverkov, V. V. Kozlov, Alexey Kryukov, 2015 .

Influence of the streamwise surface bulges upon flow separation from the wing

I. D. Zverkov, 2002, Proceedings 6th Russian-Korean International Symposium on Science and Technology. KORUS-2002 (Cat. No.02EX565).

Influence of Boundary Conditions on Properties of Stall

B. Yu. Zanin, I. D. Zverkov, 2002 .

Plasma control of vortex flow on a delta wing at high angles of attack

Victor V. Kozlov, Boris V. Postnikov, I. D. Zverkov, 2013 .

Disturbances Growth in Boundary Layers on Classical and Wavy Surface Wings

V. V. Kozlov, I. D. Zverkov, B. Zanin, 2008 .