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airfoil surface

Design and Analysis of Vortex Generator and Dimple over an Airfoil Surface to Improve Aircraft Performance

Design and Analysis of Vortex Generator and Dimple over an Airfoil Surface to Improve Aircraft Performance

... Aerodynamic efficiency is one of the most significant parameters that determine performance, weight and cost of an aircraft. Aerodynamics is critical to both commercial and military aircraft as for commercial aircrafts, ...

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Computational fluid dynamics investigation into flow behavior and acoustic mechanisms at the trailing edge of an airfoil

Computational fluid dynamics investigation into flow behavior and acoustic mechanisms at the trailing edge of an airfoil

... the surface and in high activity regions around the airfoil (such as the boundary layer and ...The airfoil surface was given the characteristics of the same material used for the physical ...

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Airfoil Flow-Separation and Stall Detection Using Surface-Mounted Pitot Tubes.

Airfoil Flow-Separation and Stall Detection Using Surface-Mounted Pitot Tubes.

... the surface of an airfoil, the airfoil can produce high lift and low ...upper surface of the airfoil separates due to a high adverse pressure gradient and the stream structure over the ...

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A Coupled Simulation Method For A Vortex-Induced Vibration System

A Coupled Simulation Method For A Vortex-Induced Vibration System

... Inverted airfoil has a low pressure suction region on the lower surface and high pressure suction region on the higher surface of airfoil ...geometry. Airfoil geometry can be summarize ...

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Investigation of Airfoil Flow Separation Control by Dielectric Barrier Discharge Plasma Actuators

Investigation of Airfoil Flow Separation Control by Dielectric Barrier Discharge Plasma Actuators

... the airfoil naturally separates from surface and the lift coefficient ...the airfoil surface, and there is a large increase in the lift coefficient ...

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Control of Transonic Shock Wave Oscillation over a Supercritical Airfoil

Control of Transonic Shock Wave Oscillation over a Supercritical Airfoil

... 2822 airfoil. The chord length, c of the airfoil is 610 ...the airfoil can be seen in Figure 1(a) and Figure 1(b) while Figure 1(c) shows the airfoil with shock control ...the airfoil ...

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Moving Surface Boundary Layer Technique For NACA 0012 Airfoil At Ultra Low Reynolds Number

Moving Surface Boundary Layer Technique For NACA 0012 Airfoil At Ultra Low Reynolds Number

... on airfoil surface for Re = 100, α = 40° is shown in Figure ...leeward surface of the airfoil and due to strong flow separation in this ...

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Lift Enhancement on Unconventional Airfoils

Lift Enhancement on Unconventional Airfoils

... Joukowsky airfoil at certain neighboring positions at which the vortex becomes ...unconventional airfoil which has cavities, corrugations or a rotating ...the airfoil surface, resulting in ...

5

Airfoil Trailing Edge Noise Generation and Its Surface Pressure Fluctuation

Airfoil Trailing Edge Noise Generation and Its Surface Pressure Fluctuation

... the surface pressure measurements is optimized for aerodynamic ...the surface pressure measurements are performed to evaluate the noise source mechanisms ...0015 airfoil, at a flow speed of 50 m/s, ...

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Active Stall Control System on NACA0012 by Using Synthetic Jet Actuator

Active Stall Control System on NACA0012 by Using Synthetic Jet Actuator

... DOI: 10.4236/jfcmv.2019.71005 68 Journal of Flow Control, Measurement & Visualization It is seen from Figure 10(a) that the leading edge vortices are not attached to the upper surface of the airfoil. A ...

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Study on Aerodynamic Characteristics of Supersonic Airfoil

Study on Aerodynamic Characteristics of Supersonic Airfoil

... supersonic airfoil, the study should focus on aerodynamic perfor- mance because a well-designed aerodynamic airfoil can distribute the load un- iformly as well as reduce air resistance to meet either ...

7

Analysis of Vertical Axis Wind Turbine Using Pitching Mechanism

Analysis of Vertical Axis Wind Turbine Using Pitching Mechanism

... Whenever the flowing medium velocity is changing with respect to a propeller, that propeller needs a pitch control mechanism to operate as desired. The wind speed always fluctuates up and down around this optimum wind ...

6

Design study of a horizontal axis tidal turbine blade

Design study of a horizontal axis tidal turbine blade

... root airfoil chord length [3] and it starts tapering towards its tip airfoil chord length [4], it also has a twist angle [16] along its entire span to keep the relative angle of attack constant (Myceket ...

220

Effect Of Spoiler Position On Aerodynamic Characteristics Of An Airfoil

Effect Of Spoiler Position On Aerodynamic Characteristics Of An Airfoil

... coordinates were taken from UIUC Airfoil data site. ANSYS fluent is reliable simulation software as many of the engineering work have been previously done by this particular program which was realistic. Many ...

6

Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment

Experimentally and CFD Analysis on Spoiler in Wind Tunnel Experiment

... upper surface relative wind velocity has to be greater than that of the lower surface relative wind. Hence pressure on the upper side of the car drops with respect to the lower surface at high ...

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Performance Analysis Of Suction Airfoil And Computational Flow Visualization Of Co-Flow Jet Airfoil

Performance Analysis Of Suction Airfoil And Computational Flow Visualization Of Co-Flow Jet Airfoil

... It is observed from the above results that, with increase in injection velocity coefficient, the flow separation is delayed. For a given chord length, the injection velocity coefficient can vary with in a certain range. ...

8

Development of Autonomous VTOL UAV for Wide Area Surveillance

Development of Autonomous VTOL UAV for Wide Area Surveillance

... analysis, airfoil, and air flow, are shown in Figure ...the airfoil for the VTOL design as shown in Figure 4, and developed the airfoil which can achieve the efficiency at a low speed, considering ...

13

Feather roughness reduces flow separation during low Reynolds number glides of swifts

Feather roughness reduces flow separation during low Reynolds number glides of swifts

... on surface roughness measurements of actual fully extended swift ...upper surface shape was measured at 37 spanwise locations with 10 mm spanwise spacing using a custom-designed 3D laser line scan set- up ...

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A NEW COMPUTATIONAL PACKAGE FOR USING IN CFD AND OTHER PROBLEMS

A NEW COMPUTATIONAL PACKAGE FOR USING IN CFD AND OTHER PROBLEMS

... Found subsidence on the undermined territo- ries of the city of Karaganda indicate geodynamic processes, which may further lead to the destruction of asphalt pavement, paludification or flooding of land, and ultimately ...

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Analytical analysis for enhancement of performance and efficiency for different blade of HAWT by computer program

Analytical analysis for enhancement of performance and efficiency for different blade of HAWT by computer program

... In the database, lift and drag coefficients for a range of angle of attack values and at low Reynolds numbers are used. One property of this database is that the only force coefficients produced in wind tunnel tests are ...

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