Results 1 to 10 of about 24,649 (162)
An alternative approach to induced drag reduction
Induced drag constitutes approximately 40% of the total drag of subsonic civil transport aircraft at cruise conditions. Various types of winglets and several non-planar concepts, such as the C-wing, the joined wings, and the box plane, have been proposed
Nikolaos Kehayas
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Wake-Model Effects on Induced Drag Prediction of Staggered Boxwings
For staggered boxwings the predictions of induced drag that rely on common potential-flow methods can be of limited accuracy. For example, linear, freestream-fixed wake models cannot resolve effects related to wake deflection and roll-up, which can have ...
Julian Schirra +2 more
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This paper analyses the nonlinear forces on a moored point-absorbing wave energy converter (WEC) in resonance at prototype scale (1:1) and at model scale (1:16).
Johannes Palm +3 more
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Numerical and Experimental Study of a Wing Combined with Wing Grids in Low Reynolds Number Flows [PDF]
One of the reasons for the increase in induced drag is the vortices created at the wing tip, which has a significant effect on reducing aerodynamic efficiency.
M. sadeghi Malekabadi, A. Banazadeh
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Substructures induced by dust drag in protoplanetary disks
Dust substructures observed in protoplanetary disks are commonly attributed to embedded planets; however, intrinsic gas-dust interactions can also generate complex morphologies.
Bi Jiaqing +4 more
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A novel approach to calculating induced drag from computational fluid dynamics
Early aerodynamic mathematical methods rely on potential flow concepts that formally isolate aerodynamic drag into a profile and an induced drag component.
George Loubimov, Michael Kinzel
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Evaluation of wing structures at the conceptual stage of transport category aircraft projects
The purpose of this research is to improve the approach for evaluating of new design solutions based on sensitivity analysis of takeoff mass (SFM) to initial changes in the basic project.
Anatolii Kretov, Dmytro Tiniakov
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Aerodynamic Modeling of a Flying Wing Featuring Ludwig Prandtl’s Bell Spanload
This paper presents the aerodynamic modeling of a flying wing featuring Ludwig Prandtl’s bell spanload. The aerodynamic models are developed using a medium fidelity vortex-lattice method and using a Reynolds-Averaged Navier–Stokes computational fluid ...
Caleb Robb, Ryan Paul
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Comparison of Induced and Parasitic Drag on Wings with Minimum Induced Drag
Minimizing the induced drag for steady level flight is a variational problem that requires solving for the optimum lift distribution given a set of design constraints. From lifting-line theory, minimizing the induced drag is, in part, achieved by varying the Fourier coefficients used to describe the section lift.
Sarah A. Abdel-Motaleb +3 more
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Developments in Wingtip Vorticity Mitigation Techniques: A Comprehensive Review
Wingtip vortices generated from aircraft wingtips, as a result of the pressure differential at the wingtip, constitute a major component of the total drag force, especially during take-off and landing.
Yousef Gharbia +3 more
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