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Swept wing

Aerodynamic Analysis of Forward Swept Wing Using Prandtl-D Wing Concept

Aerodynamic Analysis of Forward Swept Wing Using Prandtl-D Wing Concept

... PRANDTL-D WING to the forward swept wing and Aero dynamical analysis of the new wing configuration ...forward swept wings have lesser aerodynamic performance characteristics and greater ...

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On the development of controlled stationary and travelling disturbances in the supersonic boundary layer of a swept wing

On the development of controlled stationary and travelling disturbances in the supersonic boundary layer of a swept wing

... in swept-wing boundary layers has been the focus of considerable attention by researchers for more than 30 years [1, ...of swept-wing boundary layers is the presence of crossflow, which leads ...

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On the turbulent mean-flow at the leading edge of a swept wing

On the turbulent mean-flow at the leading edge of a swept wing

... a swept wing model have helped to shed some light on the minimum Reynolds number for a turbulent attachment line which is in agreement with Preston’s criterion for the flow on a flat ...

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Experimental investigation of the vorticity amplification on a swept wing with a blunt leading edge

Experimental investigation of the vorticity amplification on a swept wing with a blunt leading edge

... on swept wings [2], but the physical mechanism of interaction between freestream turbulence and boundary layer is not completely ...a swept wing plays a crucial role in establishing the initial ...

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The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing

The Aerodynamic Analysis and Aeroelastic Tailoring of a Forward-Swept Wing

... PMARC is one such code previously used at North Carolina State University and has shown excellent agreement between theoretical and experimental pressure distributions when tested on a 45 degree aft-swept ...

102

Swept wing aerodynamics at transonic speeds and at different turbulence levels

Swept wing aerodynamics at transonic speeds and at different turbulence levels

... with swept wings to attain higher critical Mach speeds which is very less in straight wing trainer ...Aircraft’s. Swept wings are preferred for its high lift to drag ratio low speed takeoff ...

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Measurement and modelling of the turbulent boundary layer near the attachment line of a swept wing

Measurement and modelling of the turbulent boundary layer near the attachment line of a swept wing

... Preston’s [20] technique was employed for the measurement of local surface shear stress. At the AL, the flow resolves into a single, spanwise velocity component, similar to the streamwise flow along a flat plate, thus ...

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Design of a swept wing High Altitude Long Endurance Unmanned Air Vehicle (HALE UAV)

Design of a swept wing High Altitude Long Endurance Unmanned Air Vehicle (HALE UAV)

... profiles, wing planforms and wing optimisation to achieve the desired performance characteristics using the Xfoil and the VSaero computational fluid dynamics (CFD) ...a wing aspect ratio of 28, ...

289

Computational Study of Aspect-Ratio Effects on Swept-Wing Stall.

Computational Study of Aspect-Ratio Effects on Swept-Wing Stall.

... Aerodynamic behavior of any lift-generating device can be broadly classified into ‘linear’ and ‘non-linear’ regimes. The linear regime is characterized by thin attached boundary layers, having a linear correlation ...

61

Computational Prediction of Tip-Vortex of a Swept Wing

Computational Prediction of Tip-Vortex of a Swept Wing

... Abstract: The near-field flow structure of a wing tip vortex behind a sweptback and tapered NACA 0015 wing was investigated using Computational Fluid Dynamics (CFD) code at Re of 1.81 x 105. In this paper, ...

9

Transonic flow past symmetrical unswept and swept wings 
		with elliptic nose

Transonic flow past symmetrical unswept and swept wings with elliptic nose

... The outer boundary of the 2D lens-type computational domain is composed by two curves   and   . The size of domain along the x axis is 80 chords; the size of domain along the y axis is 200 chords. A program written ...

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A method of reducing the drag of transport wings

A method of reducing the drag of transport wings

... a swept wing to be wholly turbulent when the flow is above some critical Reynolds ...a swept wing wind tunnel model to test this hypothesis and to check whether any useful drag saving could ...

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Wind Tunnel Investigation of Pressure Distribution and Transition Position of a Swept 3D Wing

Wind Tunnel Investigation of Pressure Distribution and Transition Position of a Swept 3D Wing

... span swept wing. The wing section had a laminar ow airfoil similar to NACA 6-series ...the wing upper surface is measured for both chordwise and spanwise ...

7

Incompressible turbulent flow at the leading edge of swept wings

Incompressible turbulent flow at the leading edge of swept wings

... There is renewed interest in low-order CFD incorporating flow control modelling as a replacement for simple data-sheet methods for use in future project studies, for which traditional design rules are not reliable. CVGK ...

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Design and Stress Analysis of Swept Back Wing with Nastran and Patran

Design and Stress Analysis of Swept Back Wing with Nastran and Patran

... a Swept Back Wing for aircraft. A swept wing is a wing that angles either backward or, occasionally, forward, from its root rather than in a straight sideways ...direction. Wing ...

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Effect of larval density and substrate quality on the wing geometry of Stomoxys calcitrans L  (Diptera: Muscidae)

Effect of larval density and substrate quality on the wing geometry of Stomoxys calcitrans L (Diptera: Muscidae)

... calcitrans wing shapes according to the dung in which flies ...calcitrans wing shape variation ...4 Wing size and adult weight of ...in wing centroid size (i), wing length (ii), ...

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Wing

Wing

... ArcMap 9.3 (ESRI 2004) and ArcToolbox 9.3 (ESRI 2008) GIS software was used for all spatial analyses. Four sets of point, line, and polygon vector databases were created in an ESRI shapefile format. Vector databases ...

11

Analysis of Low Speed Aerodynamics of Double Delta Wing

Analysis of Low Speed Aerodynamics of Double Delta Wing

... delta wing over single delta wing is that the vortices produced from “highly swept first leading edge ...highly swept strake, additional leading edge vortices are ...main wing vortices ...

7

Gliding flight: speed and acceleration of ideal falcons during diving and pull out

Gliding flight: speed and acceleration of ideal falcons during diving and pull out

... Many birds of prey attack from a high-speed dive: a fixed- wing glide along a steep, straight path. This behavior is particularly characteristic of peregrines (Falco peregrinus), falcons that strike other birds in ...

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The mechanics of wave swept algae

The mechanics of wave swept algae

... As noted previously, in the absence of flow, most nearshore algae are not noticeably streamlined. However, as a result of the structural flexibility of algal fronds, this impression can be misleading. In unidirectional ...

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