Works matching DE "HYPERSONIC aerodynamics"
Results: 554
Computational analysis of the scramjet mode of the RBCC inlet using micro vortex generators.
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- International Journal of Turbo & Jet-Engines, 2025, v. 42, n. 1, p. 1, doi. 10.1515/tjj-2024-0015
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Preparation and properties of pressureless-sintered porous Si<sub>3</sub>N<sub>4</sub>.
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- Journal of Materials Science, 2010, v. 45, n. 13, p. 3671, doi. 10.1007/s10853-010-4412-9
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The hypersonic environment: Required operating conditions and design challenges.
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- Journal of Materials Science, 2004, v. 39, n. 19, p. 5915, doi. 10.1023/B:JMSC.0000041688.68135.8b
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A correction for Reynolds‐averaged‐Navier–Stokes turbulence model under the effect of shock waves in hypersonic flows.
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- International Journal for Numerical Methods in Fluids, 2023, v. 95, n. 2, p. 313, doi. 10.1002/fld.5150
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AEROTHERMOELASTIC RESPONSE OF HYPERSONIC 2-D LIFTING SURFACE.
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- Fluctuation & Noise Letters, 2012, v. 11, n. 2, p. 1250017-1, doi. 10.1142/S0219477512500174
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General Theory of Acoustic Wave Propagation in Liquids and Gases.
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- Theoretical & Mathematical Physics, 2006, v. 146, n. 2, p. 285, doi. 10.1007/s11232-006-0024-6
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Modeling of Hypersonic Flows: Influence of the Starting Conditions of the Algorithm on the Final Solution in the Vicinity of Bifurcation Points.
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- Journal of Engineering Physics & Thermophysics, 2003, v. 76, n. 5, p. 1016, doi. 10.1023/B:JOEP.0000003215.11955.3d
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Numerical Modeling in Conjugate Formulation of the Temperature State of the Leading Edge of Hypersonic Flying Vehicles under Different Methods of Organization of the Cooling System.
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- Journal of Engineering Physics & Thermophysics, 2003, v. 76, n. 5, p. 1043, doi. 10.1023/B:JOEP.0000003218.82078.c9
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Disturbance propagation in two-dimensional boundary layers over a movable surface in the strong interaction regime.
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- Fluid Dynamics, 2011, v. 46, n. 3, p. 389, doi. 10.1134/S0015462811030045
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Supersonic low-concentration dusty-gas flow past a plane cylinder in the presence of an oblique shock wave interacting with the bow shock.
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- Fluid Dynamics, 2011, v. 46, n. 1, p. 51, doi. 10.1134/S0015462811010066
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Effect of the cone nose bluntness and the ultrasonically absorptive coating on transition in a hypersonic boundary layer.
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- Fluid Dynamics, 2010, v. 45, n. 6, p. 898, doi. 10.1134/S0015462810060074
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Numerical modeling of three-dimensional vortex structures in hypersonic transverse flow past a cylinder.
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- Fluid Dynamics, 2010, v. 45, n. 5, p. 691, doi. 10.1134/S0015462810050029
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Nonlinear wave processes in a hypersonic shock layer.
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- Fluid Dynamics, 2010, v. 45, n. 4, p. 552, doi. 10.1134/S0015462810040046
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Bispectral analysis of nonlinear processes in the hypersonic boundary layer on a porous cone surface.
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- Fluid Dynamics, 2010, v. 45, n. 3, p. 415, doi. 10.1134/S0015462810030087
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Propagation of perturbations in the three-dimensional boundary layer on a delta wing in the viscid-inviscid interaction regime.
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- Fluid Dynamics, 2010, v. 45, n. 3, p. 422, doi. 10.1134/S0015462810030099
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Interaction between an unsteady pressure disturbance and a hypersonic boundary layer.
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- Fluid Dynamics, 2009, v. 44, n. 6, p. 860, doi. 10.1134/S001546280906009X
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Thin triangular blunt-nosed plate in a viscous hypersonic flow.
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- Fluid Dynamics, 2009, v. 44, n. 4, p. 596, doi. 10.1134/S0015462809040139
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Component desorption effect on the material catalyticity in high-temperature multicomponent gases.
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- Fluid Dynamics, 2009, v. 44, n. 3, p. 453, doi. 10.1134/S0015462809030144
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Three-wave interactions between disturbances in the hypersonic boundary layer on impermeable and porous surfaces.
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- Fluid Dynamics, 2009, v. 44, n. 3, p. 362, doi. 10.1134/S0015462809030041
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Controlling the disturbances in a hypersonic flat-plate shock layer by unsteady action from the surface.
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- Fluid Dynamics, 2008, v. 43, n. 3, p. 471, doi. 10.1134/S0015462808030149
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Statistical laws of the pressure fluctuations in a hypersonic turbulent boundary layer.
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- Fluid Dynamics, 2008, v. 43, n. 2, p. 265, doi. 10.1134/S0015462808020117
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Development of slow disturbances in a hypersonic boundary layer.
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- Fluid Dynamics, 2007, v. 42, n. 5, p. 740, doi. 10.1134/S0015462807050079
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Simulation of heterogeneous atom recombination on spacecraft heat shield coatings using the methods of molecular dynamics.
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- Fluid Dynamics, 2007, v. 42, n. 4, p. 666, doi. 10.1134/S0015462807040163
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Study of the aerodynamic stability of a blunt cone with a side flap in a hypersonic flow.
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- Fluid Dynamics, 2007, v. 42, n. 1, p. 107, doi. 10.1134/S0015462807010139
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Vortex structure generation on the frontal surface of a cylinder set transversely in a hypersonic flow.
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- Fluid Dynamics, 2006, v. 41, n. 6, p. 857, doi. 10.1007/s10697-006-0101-4
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Bifurcations in the transonic flow past a symmetric airfoil.
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- Fluid Dynamics, 2006, v. 41, n. 4, p. 629, doi. 10.1007/s10697-006-0081-4
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Asymptotic solution of the two-dimensional equations for a thin viscous rarefied shock layer on a cold surface.
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- Fluid Dynamics, 2006, v. 41, n. 4, p. 633, doi. 10.1007/s10697-006-0082-3
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Study of the aerodynamic characteristics of cone-sphere models in a hypersonic flow.
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- Fluid Dynamics, 2006, v. 41, n. 3, p. 483, doi. 10.1007/s10697-006-0065-4
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Hypersonic flow past a plane magnetic dipole with parallel orientation of the magnetic moment and free-stream velocity vectors for moderate magnetic Reynolds numbers.
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- Fluid Dynamics, 2006, v. 41, n. 3, p. 475, doi. 10.1007/s10697-006-0064-5
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A method for calculating intense injection from surfaces of blunt bodies entering planetary atmospheres at hypersonic velocities.
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- Fluid Dynamics, 2006, v. 41, n. 1, p. 137, doi. 10.1007/s10697-006-0028-9
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Asymptotic Investigation of the Thin Viscous Shock Layer Equations in the Neighborhood of the Stagnation Point for Low Reynolds Numbers.
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- Fluid Dynamics, 2005, v. 40, n. 6, p. 965, doi. 10.1007/s10697-006-0011-5
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Formation of Supercritical Flow Regions on Low-Aspect-Ratio Wings.
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- Fluid Dynamics, 2005, v. 40, n. 6, p. 973, doi. 10.1007/s10697-006-0012-4
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Numerical Calculation of the Hypersonic Rarefied Transverse Flow Past a Cold Flat Plate.
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- Fluid Dynamics, 2005, v. 40, n. 5, p. 790, doi. 10.1007/s10697-005-0117-1
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Processing of Gasdynamic Numerical Solutions in Similarity Parameters.
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- Fluid Dynamics, 2005, v. 40, n. 4, p. 635, doi. 10.1007/s10697-005-0102-8
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Laminar heat exchange on sharp and blunt plates in a hypersonic air flow.
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- Fluid Dynamics, 2005, v. 40, n. 1, p. 148, doi. 10.1007/s10697-005-0053-0
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Regime diagram of the development of long-wave near-wall disturbances in a hypersonic boundary layer.
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- Fluid Dynamics, 2004, v. 39, n. 6, p. 897, doi. 10.1007/s10697-004-0006-z
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Asymptotic solution of the thin viscous shock layer equations at low reynolds numbers for a cold surface.
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- Fluid Dynamics, 2004, v. 39, n. 5, p. 815, doi. 10.1007/s10697-005-0016-5
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Hypersonic Flow Past the Spherical Nose of a Body in the Presence of a Magnetic Field.
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- Fluid Dynamics, 2004, v. 39, n. 4, p. 657, doi. 10.1023/B:FLUI.0000045682.98147.db
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Stability of the Hypersonic Shock Layer on a Flat Plate.
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- Fluid Dynamics, 2004, v. 39, n. 2, p. 181, doi. 10.1023/B:FLUI.0000030302.15633.26
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Tollmien-Schlichting Waves in a Hypersonic Boundary Layer Flow in the Neighborhood of a Cooled Surface.
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- Fluid Dynamics, 2003, v. 38, n. 2, p. 225, doi. 10.1023/A:1024269018425
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Distinctive Features of the Lateral Flow for a Convergent Air-Intake with a Convergent Nose Compression Surface.
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- Fluid Dynamics, 2002, v. 37, n. 5, p. 793, doi. 10.1023/A:1021384706044
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Physicochemical Model of Hypersonic Rarefied Gas Flow past Bodies.
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- Fluid Dynamics, 2002, v. 37, n. 4, p. 624, doi. 10.1023/A:1020601621819
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Adaptive Backstepping Control for Hypersonic Vehicles with Actuator Amplitude and Rate Saturation.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2019, v. 36, n. 2, p. 242, doi. 10.16356/j.1005-1120.2019.02.007
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Nonlinear Control Method for Hypersonic Vehicle Based on Double Power Reaching Law of Sliding Mode.
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- Transactions of Nanjing University of Aeronautics & Astronautics, 2018, v. 35, n. 5, p. 849, doi. 10.16356/j.1005-1120.2018.05.849
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On the Existence of Hypersonic Electrostatic Solitons (Estimation of Limiting Mach Numbers of Ion-Sound Solitons in a Warm Plasma).
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- Journal of Experimental & Theoretical Physics, 2020, v. 131, n. 5, p. 844, doi. 10.1134/S1063776120100040
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A Control Method for Thermal Structural Tests of Hypersonic Missile Aerodynamic Heating.
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- Mathematics (2227-7390), 2025, v. 13, n. 3, p. 380, doi. 10.3390/math13030380
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Numerical Solution of Transition to Turbulence over Compressible Ramp at Hypersonic Velocity.
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- Mathematics (2227-7390), 2023, v. 11, n. 17, p. 3684, doi. 10.3390/math11173684
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Simulations of Hypersonic Boundary-Layer Transition over a Flat Plate with the Spalart-Allmaras One-Equation BCM Transitional Model.
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- Mathematics (2227-7390), 2022, v. 10, n. 19, p. 3431, doi. 10.3390/math10193431
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Numerical Analyses and a Nonlinear Composite Controller for a Real-Time Ground Aerodynamic Heating Simulation of a Hypersonic Flying Object.
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- Mathematics (2227-7390), 2022, v. 10, n. 16, p. 3022, doi. 10.3390/math10163022
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Three-dimensional Shock Wave Interactions in Sabot Separation Launched in Hypersonic Regime.
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- Transactions of the Japan Society of Aeronautical & Space Science, 2022, v. 65, n. 4, p. 147, doi. 10.2322/tjsass.65.147
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