Results 11 to 20 of about 20,457 (265)

Estimates for the Fourier coefficients of the Duke–Imamoglu–Ikeda lift

open access: yesForum Mathematicum, 2023
Abstract Let k and n be positive even integers. For a Hecke eigenform h in the Kohnen plus subspace of weight k -
Ikeda, Tamotsu, Katsurada, Hidenori
openaire   +3 more sources

Numerical Simulation on Aerodynamics of Multi-Element Airfoil with Drooped Spoiler in Ground Effect

open access: yesXibei Gongye Daxue Xuebao, 2019
By using the finite volume method and k-ω SST turbulence model to solve the Reynolds Average Navier-Stokes equation and using the slipping wall to simulate the relative movement of the ground, the ground effect on the aerodynamic characteristic of multi ...

doaj   +1 more source

Sectional Leading Edge Vortex Lift and Drag Coefficients of Autorotating Samaras

open access: yesAerospace, 2023
Autorotating samaras such as Sycamore seeds are capable of descending at exceptionally slow speeds and the secret behind this characteristic is attributed to a flow mechanism known as the leading edge vortex (LEV).
Byung Kwon Jung, Djamel Rezgui
doaj   +1 more source

Fast Prediction of Multiple Parameters Related to Iced Airfoil Based on POD and Kriging Methods [PDF]

open access: yesJournal of Applied Fluid Mechanics, 2022
Ice accretion threatens aircraft safety. With the wide application of unmanned aerial vehicles (UAVs), the design of ice-tolerant UAVs has become a problem that must be solved.
J. Niu   +5 more
doaj   +1 more source

Weierstrass coefficients of the canonical lifting [PDF]

open access: yesInternational Journal of Number Theory, 2019
Given an ordinary elliptic curve [Formula: see text] over a field of characteristic [Formula: see text], there are functions [Formula: see text] and [Formula: see text] such that the curve [Formula: see text] where [Formula: see text] and [Formula: see text] is the canonical lifting of [Formula: see text].
openaire   +2 more sources

Wind Tunnel Experiments on an Aircraft Model Fabricated Using a 3D Printing Technique

open access: yesJournal of Manufacturing and Materials Processing, 2022
Experimental tests regarding the M-346 aircraft model made via 3D printing were carried out in order to obtain numerical data and characteristics in the form of graphs of basic aerodynamic forces and coefficients.
Katarzyna Szwedziak   +6 more
doaj   +1 more source

Lift and Drag Coefficient Map of NACA4415 Airfoil

open access: yesJournal of Physics: Conference Series, 2021
AbstractThe NACA4415 airfoil was numerically simulated with the help of the Fluent software to analyze its aerodynamic characteristics. Results are acquired as follows: The calculation accuracy of Fluent software is much higher than that of XFOIL software; the calculation result of SSTk-ω(sstkw) turbulence model is closest to the experimental value ...
Rui Yin, Jing Huang, Zhi-Yuan He
openaire   +1 more source

Experiments on the Drag and Lift Coefficients of a Spinning Sphere

open access: yesWater, 2022
The drag and lift coefficients are important parameters that affect the particle motion in a viscous fluid. In the present study, the drag and lift coefficients of a spinning sphere in a water tank were studied experimentally using a high-speed camera.
Zhou, Shuang   +2 more
openaire   +1 more source

CFD Analysis of NACA 0012 Aerofoil to Investigate the Effect of Increasing Angle of Attack on Coefficient of Lift and Coefficient of Drag

open access: yesJournal of Studies in Science and Engineering, 2022
The significance of using proper blade design is increasing with advancements in aviation technology. Wings are used in a variety of applications, including aircraft, drones, wind turbines, and more.
Mirza Haseeb Khalid
doaj   +1 more source

Numerical studies influence configuration fairing flap track airfoil type naca 4412 and naca 6412 character unmanned aerial vehicle (UAV)

open access: yesMATEC Web of Conferences, 2018
Wings have a function of changing the air flowing into force lift, and drag. It can reduce the drag is fairing flap track, where its function can reduce the obstacles caused by the effects of compressibility, fairing flap track also has a major influence
Pratama Handrico Ramelan   +1 more
doaj   +1 more source

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