Results 101 to 110 of about 3,820 (224)
This article may be downloaded for personal use only. Any other use requires prior permission of the author and AIP Publishing. This article appeared in (Hu, X., An, B., Guan, Y., Li, D., Mellibovsky, F., Sang, W., & Wang, G. (2025).
An, Bo +6 more
core +1 more source
A STUDY FOR AERODYNAMIC DESIGN OPTIMIZATION OF AIRFOIL USING e-SCIENCE BASED AERODYNAMIC DESIGN OPTIMIZATION FRAMEWORK [PDF]
In this study, aerodynamic design optimization of airfoil was performed to minimize drag of baseline airfoil at transonic flow by using e-Science based design framework.
유민석 +3 more
core
Weight indexing for airfoil multi-objective optimization
A new method for airfoil shape optimization is presented, in which the airfoil shape is optimized not only for the best aerodynamic efficiency but also for the minimum structural weight.
Tooren, M.J.L.V., Elham, A.
core +1 more source
Airfoil design by optimization
An airfoil design technique is described which uses an analytical method for representing the airfoil contour by Wagner functions and a computational procedure for obtaining the values of the coefficients of expansion.
Ramamoorthy, P, Padmavathi, K
core
Kriging-Based Variable Screening Method for Aircraft Optimization Problems with Expensive Functions
The computational complexity of airfoil optimization for aircraft wing designs typically involves high-dimensional parameter spaces defined by geometric variables, where each Computational Fluid Dynamics (CFD) simulation cycle may require significant ...
Yadong Wang +4 more
doaj +1 more source
Airfoil aerodynamic design represents an essential domain in aircraft development, where the pursuit of advanced and intelligent optimization strategies is important for achieving significant advancements.
Yiting Zhang +3 more
doaj +1 more source
Optimization of Long-Endurance Airfoils [PDF]
Jun Hua +3 more
openaire +1 more source
The highly nonlinear aerodynamic interference in tandem-airfoil configurations significantly hinders the precise exploitation of their aerodynamic potential.
Haijun Gong +4 more
doaj +1 more source
This paper describes a new integrated approach for the multi-disciplinary optimization of a entry capsule’s shape. Aerothermodynamics, Flight Mechanics and Thermal Protection System behaviour of a reference spaceship when crossing Martian atmosphere are ...
Gallizio, Federico +6 more
core
Wave Drag Reduction of SC(2)0410 Airfoil using New Developed Inviscid Compressible Adjoint Method
A supercritical airfoil is geometrically optimized using the new developed adjoint compressible lattice Boltzmann method. Minimizing the drag coefficient and eliminating the shock wave on the supercritical airfoil surface are considered as the cost ...
R. Kamali-Moghadam +2 more
doaj

