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NTIS 바로가기Experimental thermal and fluid science : ETF science, v.85, 2017년, pp.213 - 228
Lo, K.H. , Kontis, K.
An experimental study has been conducted to investigate the flow characteristics over two rounded contour bumps. Vane-type vortex generators or longitudinal aligned passive by-pass jets were implemented in attempt to achieve wake flow control in rounded contour bumps. According to the results collec...
Byun 2005 Structure of Three-Dimensional Separated Flow on Symmetric Bumps
AIAA J. Byun 42 4 754 2004 10.2514/1.1829 Study of vortical separation from three-dimensional symmetric bumps
Int. J. Heat Fluid Flow Yakeno 55 52 2015 10.1016/j.ijheatfluidflow.2015.07.014 Separation control based on turbulence transition around a two-dimensional hump at different Reynolds numbers
Iaccarino 389 2003 RANS Simulation of the Separated Flow Over a Bump with Active Control
Lo 2014 Experimental Studies on Contour Bumps and Cavities at Supersonic Speed
Exp. Therm. Fluid Sci. Lo 80 228 2017 10.1016/j.expthermflusci.2016.08.027 Flow characteristics of various three-dimensional rounded contour bumps in a Mach 1.3 freestream
Acta Astronaut. Lo 126 229 2016 10.1016/j.actaastro.2016.04.033 Control of flow separation on a contour bump by jets in a Mach 1.9 freestream: an experimental study
J. Visual. Lo 2016 Flow visualisation of a normal shock impinging over a rounded contour bump in a Mach 1.3 free-stream
AIAA J. Eastwood 50 12 2882 2012 10.2514/1.J051740 Toward designing with three-dimensional bumps for lift/drag improvement and buffet alleviation
10.1007/978-3-540-74460-3_10 B. König, M. Pätzold, T. Lutz, E. Krämer, Shock control bumps on flexible and trimmed transport aircraft in Transonic Flow, in: New Results in Numerical and Experimental Fluid Mechanics VI, Notes on Numerical Fluid Mechanics and Multidisciplinary Design (NNFM), vol. 96, 2007, pp. 80-87.
J. Aircraft König 46 2 675 2009 10.2514/1.41441 Numerical and experimental validation of three-dimensional shock control bumps
Proc. IMech E Part G J. Aerosp. Eng. Qin 222 5 619 2008 10.1243/09544100JAERO333 Three-dimensional contour bumps for transonic wing drag reduction
J. Aerosp. Sci. Technol. Wong 12 436 2008 10.1016/j.ast.2007.10.011 A combined experimental and numerical study of flow structures over three-dimensional shock control bumps
P.C. Simon, D.W. Brown, R.G. Huff, Performance of External-Compression Bump Inlet at Mach Numbers of 1.5 and 2.0, NACA Report, NACA-RM-E56L19, 1957.
Svensson 2013 A CFD Investigation of a Generic Bump and Its Application to a Diverterless Supersonic Inlet
Exp. Fluids Chen 56 11 1 2015 10.1007/s00348-015-2077-5 Passive jet control of flow around a circular cylinder
ASCE, J. Aerosp. Eng. Chen 2016 A passive jet flow control method for suppressing unsteady vortex shedding from a circular cylinder
Lu 2011 Proceedings of 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, United States, 4-7 January 2011 Review of micro vortex generators in high-speed flow
AIAA J. Herges 48 11 2529 2010 10.2514/1.J050313 Microramp flow control of normal shock/boundary-layer interactions
Prog. Aerosp. Sci. Lin 38 389 2002 10.1016/S0376-0421(02)00010-6 Review of research on low-profile vortex generators to control boundary layer separation
AIAA J. Babinsky 47 3 668 2009 10.2514/1.38022 Microramp control of supersonic oblique shock-wave/boundary-layer interactions
J. Aircraft Li 47 6 2086 2010 10.2514/1.C000318 Declining angle effects of the trailing edge of a microramp vortex generator
Flow Meas. Instrum. Zare-Behtash 2017 Pressure sensitive paint measurements at high Mach numbers
AIAA J. Kontis 44 12 2962 2006 10.2514/1.21018 Compressible vortex-ring interaction studies with a number of generic body configurations
Phys. Fluids Kontis 20 1 016104 2008 10.1063/1.2837172 Head-on collision of shock wave induced vortices with solid and perforated walls
Shock Waves Kontis 17 5 323 2008 10.1007/s00193-007-0114-x Effect of dimples on glancing shock wave turbulent boundary later interactions
Sensors Actuat. B: Chem. Yang 161 1 100 2012 10.1016/j.snb.2011.09.053 Application of AA-PSP to hypersonic flows: the double ramp model
Micromachines Saad 3 2 364 2012 10.3390/mi3020364 Micro-ramps for hypersonic flow control
Int. J. Heat Fluid Flow Yang 37 9 2012 10.1016/j.ijheatfluidflow.2012.05.004 Pressure-sensitive paint on a truncated cone in hypersonic flow at incidences
Int. J. Heat Fluid Flow Zare-Behtash 30 3 561 2009 10.1016/j.ijheatfluidflow.2009.02.022 Compressible vortex loops: effect of nozzle geometry
Int. J. Heat Fluid Flow Zare-Behtash 32 3 596 2011 10.1016/j.ijheatfluidflow.2011.02.013 Effect of primary jet geometry on ejector performance: a cold-flow investigation
Exp. Therm. Fluid Sci. Yang 40 50 2012 10.1016/j.expthermflusci.2012.01.032 Investigation of the double ramp in hypersonic flow using luminescent measurement systems
Exp. Therm. Fluid Sci. Ukai 52 59 2013 10.1016/j.expthermflusci.2013.08.022 Effectiveness of jet location on mixing characteristics inside a cavity in supersonic flow
Int. J. Heat Fluid Flow Ukai 50 254 2014 10.1016/j.ijheatfluidflow.2014.08.009 Effects of dual jets distance on mixing characteristics and flow path within a cavity in supersonic crossflow
Int. J. Heat Fluid Flow Zare-Behtash 53 146 2015 10.1016/j.ijheatfluidflow.2015.03.004 Transverse jet-cavity interactions with the influence of an impinging shock
Lusk 2011 Control of Supersonic Cavity Flow by Leading Edge Blowing
Lusk 2011 Proceedings of 49th AIAA Aerospace Sciences Meeting Including the New Horizons Forum and Aerospace Exposition, Orlando, Florida, United States, 4-7 January, 2011 Flow field effects on control on supersonic open cavities
Exp. Fluid Lusk 53 187 2012 10.1007/s00348-012-1282-8 Leading edge slot blowing on an open cavity in supersonic flow
J. Wind Eng. Indust. Aerodyn. Lo 159 110 2016 10.1016/j.jweia.2016.10.009 Flow characteristics over a tractor-trailer model with and without vane-type vortex generator installed
Exp. Therm. Fluid Sci. Lo 82 58 2017 10.1016/j.expthermflusci.2016.11.003 Flow around an articulated lorry model
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