Results 161 to 170 of about 21,879 (220)

Numerical Investigation of an NACA 13112 Morphing Airfoil. [PDF]

Biomimetics (Basel)
Feraru MD, Măriuța D, Stoia-Djeska M, Grigorie LT.   +3 more
europepmc   +1 more source

Efficient Exothermic Press toward Ultrafast and Scalable Manufacturing of Complex Polymer Composites. [PDF]

Adv Sci (Weinh)
Tarafdar A, Zhang H, Wang X, Hoe AJ, Deng K, Fu K, Qiao Q, Hosein ID, Wang Y.   +8 more
europepmc   +1 more source

A numerical assessment of the heterogeneous effects of innovative shroud profiles for horizontal axis wind turbine. [PDF]

Heliyon
Hamid H, Abd El Maksoud RM.
europepmc   +1 more source

Bifurcation and synchronization analysis in a stall-flutter aeroelastic system under varying preset angles and frequency ratios. [PDF]

Sci Rep
Kumar S, Venkatramani J, Gupta A.
europepmc   +1 more source

Multi-slotted airfoil design for enhanced aerodynamic performance and economic efficiency. [PDF]

Sci Rep
Aziz MA, Khalifa MA, Abdelrahman MA, Elshimy H, Elsayed AM.   +4 more
europepmc   +1 more source

Aerodynamic Investigation on a Coaxial-Rotors Unmanned Aerial Vehicle of Bionic Chinese Parasol Seed. [PDF]

Biomimetics (Basel)
Gan W, Wang Y, Wang H, Zhuang J.
europepmc   +1 more source

Laser-Engraved Micro-Patterned rGO/WPU Composite Structures for Aircraft Applications: Synchronizing Electrothermal De-Icing and Broadband Microwave Transparency. [PDF]

Adv Sci (Weinh)
Fu X, Shen Y, Zhao L, Zhu W, Liu W, Li C, Lin Y, Ye Z, Shen C.   +8 more
europepmc   +1 more source

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Airfoil optimization by Evolution Strategies

2013 IEEE Congress on Evolutionary Computation, 2013
This paper addresses subsonic airfoil optimization using Evolution Strategies (ES) and devises a means of defining the airfoil geometry that reduces unnecessary restrictions in the search space. The solution encoding uses Bezier Control Points to define the geometry of the airfoil, but does not restrict the movement of the control points as was common ...
Drew A. Curriston, Alice E. Smith
openaire   +1 more source

Airfoil design by optimization

Journal of Aircraft, 1977
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. The method for approximating an airfoil contour by a Fourier-type series of Wagner functions is briefly outlined, and a flow chart for ...
P. Ramamoorthy, K. Padmavathi
openaire   +1 more source