Contents

Mathematical Models and Computer Simulations

Vol. 15, No. 1, 2023

Implicit-Explicit Bicompact Schemes for Hyperbolic Systems of Conservation Laws

M. D. Bragin p. 1  abstract

Accounting for Stimulation Treatments in Modeling the Development of Oil Reservoirs Using the Material Balance Method

A. D. Bekman p. 13  abstract

A 2D Model for Calculating the Radiational Electromagnetic Induction in a Coaxial Cable Line

A. V. Sysenko p. 23  abstract

Approximate Integration of Ordinary Differential Equations Using the Chebyshev Series with Precision Control

S. F. Zaletkin p. 34  abstract

Comparison of Relative Motion Models for Spacecraft Flying in Formation

I. A. Suslova, Y. V. Mashtakov and S. A. Shestakov p. 47  abstract

Investigation of Vortex Structures in the Supersonic Flow around a Tandem of Wings

V. E. Borisov, T. V. Konstantinovskaya and A. E. Lutsky p. 59  abstract

Mathematical Modeling and Optimization of the Process of Formation of Functional Thin MoSe2 Films

V. A. Majidzade, G. S. Aliyev, S. P. Javadova, A. Sh. Aliyev, S. D. Dadashova and D. B. Tagiyev p. 73  abstract

Computational and Experimental Studies of a Low-Noise Aircraft with a Laminar Wing and Engines above the Trailing Edge of the Wing

A. L. Bolsunovsky, N. N. Bragin, N. P. Buzoverya, E. S. Perchenkov, I. L. Chernyshev and S. I. Skomorokhov p. 79  abstract

Approaches to the Numerical Simulation of the Acoustic Field Generated by a Multi-Element Aircraft Wing in High-Lift Configuration

A. V. Gorobets, A. P. Duben, T. K. Kozubskaya and P. V. Rodionov p. 92  abstract

Numerical Simulation of the Evolution of an Intense Aerodynamic Jet in the Far-Field of Propagation

S. N. Gurbatov, I. Yu. Demin, A. A. Lisin, S. A. Karabasov and A. V. Tyurina p. 109  abstract

Numerical Simulation of the Evolution of Turbulent Spots in a Supersonic Boundary Layer over a Plate

I. V. Egorov, A. V. Novikov and P. V. Chuvakhov p. 118  abstract

Development of Unstructured Code for Rotating Zones Based on the Cabaret Method with Improved Spectral Properties

I. A. Solntsev and S. A. Karabasov p. 125  abstract

Mathematical Modeling as an Integral Part of Wind Tunnel Experimental Methodology

S. M. Bosnyakov, M. F. Engulatova, S. V. Matyash and S. V. Mikhaylov p. 138  abstract

Function Approximation Technique (FAT)-Based Adaptive Feedback Linearization Control for Nonlinear Aeroelastic Wing Models Considering Different Actuation Scenarios

Hayder F. N. Al-Shuka and B. Corves p. 152  abstract