В. Н. Усков

477 total citations
36 papers, 364 citations indexed

About

В. Н. Усков is a scholar working on Computational Mechanics, Applied Mathematics and Aerospace Engineering. According to data from OpenAlex, В. Н. Усков has authored 36 papers receiving a total of 364 indexed citations (citations by other indexed papers that have themselves been cited), including 27 papers in Computational Mechanics, 17 papers in Applied Mathematics and 15 papers in Aerospace Engineering. Recurrent topics in В. Н. Усков's work include Computational Fluid Dynamics and Aerodynamics (23 papers), Gas Dynamics and Kinetic Theory (14 papers) and Fluid Dynamics and Turbulent Flows (12 papers). В. Н. Усков is often cited by papers focused on Computational Fluid Dynamics and Aerodynamics (23 papers), Gas Dynamics and Kinetic Theory (14 papers) and Fluid Dynamics and Turbulent Flows (12 papers). В. Н. Усков collaborates with scholars based in Russia, United States and China. В. Н. Усков's co-authors include М. В. Чернышов, М.V. Silnikov, П. В. Булат and V. N. Malozemov and has published in prestigious journals such as Acta Astronautica, Shock Waves and Journal of Applied Mathematics and Mechanics.

In The Last Decade

В. Н. Усков

33 papers receiving 323 citations

Peers

Countries citing papers authored by В. Н. Усков

Since Specialization

Citations

This map shows the geographic impact of В. Н. Усков's research. It shows the number of citations coming from papers published by authors working in each country. You can also color the map by specialization and compare the number of citations received by В. Н. Усков with the expected number of citations based on a country's size and research output (numbers larger than one mean the country cites В. Н. Усков more than expected).

Fields of papers citing papers by В. Н. Усков

Since Specialization

Physical SciencesHealth SciencesLife SciencesSocial Sciences

This network shows the impact of papers produced by В. Н. Усков. Nodes represent research fields, and links connect fields that are likely to share authors. Colored nodes show fields that tend to cite the papers produced by В. Н. Усков. The network helps show where В. Н. Усков may publish in the future.

Co-authorship network of co-authors of В. Н. Усков

This figure shows the co-authorship network connecting the top 25 collaborators of В. Н. Усков. A scholar is included among the top collaborators of В. Н. Усков based on the total number of citations received by their joint publications. Widths of edges represent the number of papers authors have co-authored together. Node borders signify the number of papers an author published with В. Н. Усков. В. Н. Усков is excluded from the visualization to improve readability, since they are connected to all nodes in the network.

All Works

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20 of 20 papers shown

#	Work	Indexed citations
1	Gas-dynamic Waves and Discontinuities 2016 ·П. В. Булат, В. Н. Усков	0
2	Classification of Gas-dynamic Discontinuities and their Interference Problems 2014 ·Research Journal of Applied Sciences Engineering and Technology ·В. Н. Усков, П. В. Булат, (unknown)	14
3	The problem of constructing the optimal configuration of shock and detonation waves 2014 ·В. Н. Усков, П. В. Булат	0
4	Shock and detonation wave in terms of view of the theory of interaction gasdynamic discontinuities 2014 ·В. Н. Усков, П. В. Булат	21
5	Two-dimensional over-expanded jet flow parameters in supersonic nozzle lip vicinity 2014 ·Acta Astronautica ·М.V. Silnikov, М. В. Чернышов, В. Н. Усков	34
6	Extreme shockwave systems in problems of external supersonic aerodynamics 2014 ·Thermophysics and Aeromechanics ·В. Н. Усков, М. В. Чернышов	12
7	Analytical solutions for Prandtl–Meyer wave–oblique shock overtaking interaction 2014 ·Acta Astronautica ·М.V. Silnikov, М. В. Чернышов, В. Н. Усков	49
8	On classification of flow regimes in a channel with sudden expansion 2012 ·Thermophysics and Aeromechanics ·П. В. Булат, (unknown), В. Н. Усков	7
9	Interference of stationary and non-stationary shock waves 2010 ·Shock Waves ·В. Н. Усков, (unknown)	10
10	Triple configurations of traveling shock waves in inviscid gas flows 2008 ·Journal of Applied Mechanics and Technical Physics ·В. Н. Усков, (unknown)	9
11	Special and extreme triple shock-wave configurations 2006 ·Journal of Applied Mechanics and Technical Physics ·В. Н. Усков, М. В. Чернышов	37
12	Differential characteristics of the flow field in a plane overexpanded jet in the vicinity of the nozzle lip 2006 ·Journal of Applied Mechanics and Technical Physics ·В. Н. Усков, М. В. Чернышов	9
13	An approximate analytical model of flow in the first barrel of an overexpanded jet 2003 ·Technical Physics Letters ·(unknown), В. Н. Усков, (unknown)	12
14	Interference of nonstationary oblique shock waves 2002 ·Technical Physics Letters ·(unknown), В. Н. Усков	4
15	Analysis of the Acoustic Impedance in Stationary Supersonic Flows 1998 ·Journal of Engineering Physics and Thermophysics ·(unknown), (unknown), В. Н. Усков	2
16	The minimization of the total pressure loss accompanying the breakdown of a supersonic flow 1998 ·Journal of Applied Mathematics and Mechanics ·V. N. Malozemov, (unknown), В. Н. Усков	2
17	Maximum turning angles of a supersonic flow in shock-wave systems 1998 ·Fluid Dynamics ·(unknown), В. Н. Усков	6
18	An optimal shock-expansion system in a steady gas flow 1997 ·Journal of Applied Mechanics and Technical Physics ·(unknown), В. Н. Усков	7
19	Optimal shock-wave systems 1995 ·Fluid Dynamics ·(unknown), В. Н. Усков	18
20	Interference of steady shock waves traveling in the same direction 1987 ·Fluid Dynamics ·(unknown), (unknown), В. Н. Усков	2

Rankless uses publication and citation data sourced from OpenAlex, an open and comprehensive bibliographic database. While OpenAlex provides broad and valuable coverage of the global research landscape, it—like all bibliographic datasets—has inherent limitations. These include incomplete records, variations in author disambiguation, differences in journal indexing, and delays in data updates. As a result, some metrics and network relationships displayed in Rankless may not fully capture the entirety of a scholar's output or impact.

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