[PDF] Top 20 Numerical and experimental investigations of the supersonic microramp wake
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Numerical and experimental investigations of the supersonic microramp wake
... the supersonic regime, the use of MVG is largely associated to the control of shock wave/boundary layer interactions (SWBLI), a phenomenon occurring in supersonic inlets among other ...Several ... See full document
29
Experimental investigations and numerical simulations of methane cup-burner flame
... of experimental investigations and numerical ...by numerical simulations. Qualitative agreement between experimental and predicted oscillatory behaviour was obtained by employing a ... See full document
5
Numerical and experimental investigations of buffet on a diamond airfoil designed for space launchers applications
... some numerical and experimental investigations about the aerodynamic and aero-elastic behavior of a diamond airfoil, designed for microsatellite-dedicated launchers, with a particular interest for ... See full document
15
Numerical and experimental investigations of buffet on a diamond airfoil designed for space launcher applications
... It is thus necessary to predict the loads induced by the buffeting, to ensure that structure components and subsystems have adequate strength, stress and fatigue margins in regard to the structural dynamic response. ... See full document
17
Numerical and Experimental Investigations on Vertical Axis Wind Turbines of Different Models
... Wind is a free and abundant energy source and conversion of wind energy to electrical energy has no negative impact to the environment. Though the harvest of energy using a horizontal axis turbine (HAWT) is extremely ... See full document
37
Numerical and Experimental Investigations for Design of a High Performance Micro-hydro-kinetic Turbine
... 4. 1. Transient Simulation of Propeller's Dynamics with One-dimensional Actuator-disc Method The fluid flow was governed with one- dimensional quasi-transient equations which were obtained after integration from ... See full document
6
Numerical and Experimental Investigations of the Effect of Melt Delivery Nozzle Design on the Open- to Closed-Wake Transition in Closed-Coupled Gas Atomization
... The experimental and CFD studies show that the most significant difference in WCP was observed between nozzle types 1 and ...the experimental and CFD study this nozzle was observed to have a WCP of ... See full document
47
Numerical and experimental investigations of self piercing riveting
... There have been a few published results on the static and dynamic properties of the SPR joints in the past few years. Wood et al. [3] investigated the performance of self- piercing riveted joints in aluminium sheet ... See full document
14
Numerical investigation of transitional supersonic axisymmetric wakes
... Transitional supersonic axisymmetric wakes are investigated by conducting various numerical ...direct numerical simulations (DNS), a linearized N-S code for linear stability investigations ... See full document
41
Investigations of Supersonic Flow Around a Long Axisymmetric Body
... The numerical scheme used was implicit Beam and Warming central dierencing, while a Baldwin-Lomax turbulence model was used to close the Reynolds Averaged Navier-Stokes (RANS) ...some experimental ones ... See full document
11
Numerical Investigations on Supersonic Fluid Flow past a Cavity Relating Coefficient of Pressure and Density Fields
... conducted numerical simulations of fluidic control for transonic cavity ...of supersonic open cavity ...of supersonic flow over two dimensional ...the experimental study on double-cavity ... See full document
7
Experimental and Numerical Investigations of Forced Convection in Tube-Type Heat Exchanger
... Velocity patternin the bank isillustrated in Fig.7. Fluid velocity in the mid-plane of the tubes wasobserved to be higher and weak near tube surface plane because of the boundary layer development on the surface. A ... See full document
10
A Numerical Solution to the Inverse Problem of Supersonic-Nozzle Design
... The numerical algorithm of supersonic-nozzle de- sign is particularly sensitive to stability in the region of su- personic flow ([1 ] to [5]). Although the application of nu- merical methods is very common ... See full document
8
Experimental and numerical investigations into the underwater explosion induced whipping response of submerged platforms
... the experimental setup did not provide a sufficient way to track the shape and motion of the ...other experimental work discussed in Chapter 2, particularly the noted observations from Krieger and Chahine ... See full document
162
Experimental and numerical investigations of oil film formation and friction in a piston ring-liner contact
... all-regime numerical model is used to predict the pressure profile, film thickness and friction ...The experimental results were compared to the numerical ... See full document
18
Experimental and numerical investigations of primary flow patterns and mixing in laboratory meandering channel
... In this research, velocity profiles of experiment method and numerical simulation have been com-pared and analyzed with same hydraulic conditions. The depth-averaged primary velocity vector field of the ... See full document
15
Experimental and numerical investigations into the underwater explosion induced whipping response of submerged platforms
... the numerical model does contain endcaps and is therefore expected to have slightly lower natural frequencies compared to the uniform cylinder due to the additional ... See full document
27
Theoretical, Experimental and Numerical Investigations of the Effect of Inlet Blade Angle on the Performance of Regenerative Blowers
... and numerical CFD technique using CFX-ANSYS 16.1 are done. The numerical CFD analysis show that the flow enters the impeller from the blade side (about 65% of the blade side area) and leaves from the blade ... See full document
14
Experimental and Numerical Investigations on Al2O3–Tricosane Based Heat Pipe Thermal Energy Storage
... module was explained in literature [13]. The heat pipe cooling system is composed of three components viz. evaporator, energy storage tank (adiabatic section) and condenser. Experiments were conducted at different ... See full document
6
The Vortical Structures in the Rear Separation and Wake Produced by a Supersonic Micro-Ramp
... the wake of the micro-ramp, a momentum deficit is at the center and a curved shear layer is then formed between the deficit region and free ...the wake has been substantially discussed by Sun et al 8 ...the ... See full document
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