A. N. Shiplyuk - Concepedia

Author

A. N. Shiplyuk

Institute of Theoretical and Applied Mechanics

Also Known As

A N Shiplyuk, A Shiplyuk, A. N. SHIPLYUK, A. N. Shiplyuk, A. SHIPLYUK, A. Shiplyuk, A.N Shiplyuk, A.N. Shiplyuk, Alexander N. Shiplyuk, Alexander Shiplyuk

101

Publications

1.6K

Citations

H-Index

Concepts

All Affiliations

Institute of Theoretical and Applied Mechanics Russian Academy of Sciences Rockwell Automation (United States)Moscow Institute of Physics and Technology Novosibirsk State Technical University

About

A. N. Shiplyuk is an author at Institute of Theoretical and Applied Mechanics specializing in engineering, space engineering, and aerodynamics.

Top Concepts

#	Concept	H-Index	Publications	Citations
1	Engineering	16	24	951
2	Mechanical Engineering	10	10	326
3	Materials Science	5	5	237
4	Applied Physics	3	3	134
5	Mechanics	1	1	10

A. N. Shiplyuk

Publications

1.4K

Citations

H-Index

Page 1

	Year	Citations
Stabilization of a hypersonic boundary layer using an ultrasonically absorptive coating A. N. Shiplyuk, E. V. Burov, Norman Malmuth Journal of Fluid Mechanics	2003	241
Leading-edge receptivity of a hypersonic boundary layer on a flat plate A. N. Shiplyuk, A. A. Sidorenko, D. Arnal Journal of Fluid Mechanics AeroacousticsHypersonic Boundary LayerEngineeringFlat PlateWave Motion	2001	154
Stability of Hypersonic Boundary Layer on Porous Wall with Regular Microstructure V. E. Kozlov, A. N. Shiplyuk, Norman Malmuth AIAA Journal AeroacousticsHypersonic Boundary LayerPorous WallEngineeringFluid Mechanics	2006	100
Nonlinear Aspects of Hypersonic Boundary-Layer Stability on a Porous Surface Ndaona Chokani, D. A. Bountin, A. N. Shiplyuk AIAA Journal Materials ScienceVibrationsEngineeringPower UltrasoundPhysical Acoustic	2005	99
Evolution of nonlinear processes in a hypersonic boundary layer on a sharp cone D. A. Bountin, A. N. Shiplyuk Journal of Fluid Mechanics Nonlinear ProcessesAeroacousticsHypersonic Boundary LayerEngineeringPhysics	2008	81
Hydrogen-fueled detonation ramjet model: Wind tunnel tests at approach air stream Mach number 5.7 and stagnation temperature 1500 K V. S. Ivanov, V. S. Aksenov, D. A. Vnuchkov, International Journal of Hydrogen Energy EngineeringDetonation PhenomenonAerospace EngineeringWind Tunnel TestsAerodynamics	2018	78
Hypersonic Laminar Flow Control Using a Porous Coating of Random Microstructure A. N. Shiplyuk, Andrew Sidorenko, V. F. Kozlov, 44th AIAA Aerospace Sciences Meeting and Exhibit Tribological CoatingAeroacousticsEngineeringFlow ControlFluid Mechanics	2006	52
Stabilization of High-Speed Boundary Layer Using Porous Coatings of Various Thicknesses A. N. Shiplyuk, Vitaly Soudakov AIAA Journal Hypersonic Boundary LayerEngineeringFluid MechanicsMechanical EngineeringBoundary Layer	2012	51
Influence of a Counterflow Plasma Jet on Supersonic Blunt-Body Pressures Norman Malmuth, A. P. Shashkin, T. A. Korotaeva, AIAA Journal AeroacousticsUnsteady FlowEngineeringAerospace EngineeringFluid Mechanics	2002	51
Experimental study of the effect of a passive porous coating on disturbances in a hypersonic boundary layer 2. Effect of the porous coating location S. O. Morozov, A. N. Shiplyuk Journal of Applied Mechanics and Technical Physics	2016	48

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