I. I. Mazhul’

发表

Numerical modeling of the conditions for realization of flow regimes in supersonic axisymmetric conical inlets of internal compression

Yu. P. Gounko, I. I. Mazhul’, Y. Gounko, 2015 .

Flow field study in the T-313 wind-tunnel test section for M = 7

A. I. Maksimov, I. I. Mazhul’, V. Zapryagaev, 2013 .

Numerical investigation of off-design regimes of flow past waveriders on the basis of axisymmetric conical flows

I. I. Mazhul’, R. Rakhimov, 2007 .

Numerical Investigation of Off-Design Regimes of Flow Past Power-Law Waveriders Based on the Flows Behind Plane Shocks

I. I. Mazhul’, R. Rakhimov, 2003 .

Numerical simulation of starting conditions for a supersonic air intake with a rectangular duct and partial release of the captured air stream through longitudinal slots

I. I. Mazhul’, Y. Gounko, 2022, Thermophysics and Aeromechanics.

Structure of Flow over a Hypersonic Inlet with Side Compression Wedges

I. I. Mazhul, A. F. Latypov, P. Rostand, 2003 .

Gasdynamic design of a two-dimensional supersonic inlet with the increased flow rate factor

I. I. Mazhul, Yu. P. Gounko, I. I. Mazhul’, 2012 .

Numerical Investigation of Supersonic Flows Around Hyperelliptic Cones

I. I. Mazhul’, V. Volkov, 2001 .

Supersonic flow in the rectangular duct of an air inlet with the separation-induced interaction of the boundary layer with shock waves

I. I. Mazhul’, 2020, Thermophysics and Aeromechanics.

Numerical simulation of a three-dimensional flow in a channel with interaction of a plane shock wave and a longitudinally ribbed surface

I. I. Mazhul’, 2021, Thermophysics and Aeromechanics.

Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inlet

I. I. Mazhul’, Y. Gounko, 2018 .

Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet

I. I. Mazhul’, Y. Gounko, 2018 .

Aerodynamic design and experimental modelling of an innovative supersonic three-dimensional air-intake

I. I. Mazhul’, A. Kharitonov, Y. Gounko, 2013, The Aeronautical Journal (1968).

Experimental characteristics of a supersonic three-dimensional air inlet with adjustable throat

I. I. Mazhul’, Y. Gounko, 2013 .

Gasdynamic design of a two-dimensional supersonic inlet with the increased flow rate factor

I. I. Mazhul’, Y. Gounko, 2012, Thermophysics and Aeromechanics.

Numerical investigation of supersonic flow breakdown at the inlet duct throttling

I. I. Mazhul’, Y. Gounko, V. I. Nurutdinov, 2014, Thermophysics and Aeromechanics.

Gasdynamic and turbulent features of flows with a pseudo-shock wave in axisymmetric ducts

I. I. Mazhul’, Y. Gounko, 2018 .

Flow turbulization in a pseudo-shock forming in an axisymmetric duct with a frontal inlet

I. I. Mazhul’, Y. Gounko, 2018, Thermophysics and Aeromechanics.

Numerical simulation of the flow with a pseudo-shock in an axisymmetric expanding duct with a frontal inlet

I. I. Mazhul’, Y. Gounko, 2018, Thermophysics and Aeromechanics.

Hypersonic Power-Law Shaped Waveriders in Off-Design Regimes

I. I. Mazhul, I. I. Mazhul’, R. D. Rakchimov, 2004 .