Results 101 to 110 of about 36,102 (211)

Constructal theory of aerodynamic design in NACA airfoils for search and rescue UAVs using integrated CFD and ANN approaches. [PDF]

Sci Rep
Shbailat SJ, Ridha HD.
europepmc   +1 more source

Enhancing performance of gravitational water vortex turbines through airfoil design and basin parameters. [PDF]

Sci Rep
Michel M, Alaktaa AH, Elsherbiny K, Mehanna A, Shehata AS.   +4 more
europepmc   +1 more source

Numerical investigation on aerodynamic characteristics of a tiltrotor wing with serrated Gurney flap. [PDF]

Sci Rep
Chen H.
europepmc   +1 more source

CFD-driven neural network and SVM models for airfoil aerodynamic enhancement with bio-inspired riblets and plasma actuation. [PDF]

Sci Rep
Karthikeyan KV, Raju A, Jain J, Lekshmanan S, Rajan H.   +4 more
europepmc   +1 more source

Pemilihan Profil Sayap Pesawat LSU-02 NG LD Dengan Menggunakan Metode Panel (Choise Wing Profile Of LSU-02 NG LD Aircraft With Panel Methode)

, 2018
Telah dilakukan pemilihan airfoil untuk profil sayap pesawat LSU-02 NG LD. Kandidat dari airfoil tersebut diantaranya FX63-120, GOE 501, dan GOE 497 serta ada tambahan airfoil yang merupakan airfoil yang digunakan oleh pesawat pembanding (Penguin C ...
Dana Herdiana, Arifin Rasyadi S.
core  

Numerical investigation of co-flow jet integration to enhance the aerodynamic efficiency of airfoils used in wind turbine applications. [PDF]

Sci Rep
Farghaly MB, El Kader OMA, Alsharif AMA, Halawa M.   +3 more
europepmc   +1 more source

SuperWing: a comprehensive transonic wing dataset for data-driven aerodynamic design. [PDF]

Sci Data
Yang Y, Tang W, Liu M, Thuerey N, Zhang Y, Chen H.   +5 more
europepmc   +1 more source

The transonic safe mode as an enabler of next-generation wind turbines. [PDF]

Commun Eng
De Tavernier DAM, Zaaijer MB, von Terzi DA.   +2 more
europepmc   +1 more source

Study on wind resistance performance of high-rise corridor building based on quasi-steady static aeroelastic analysis method. [PDF]

Sci Rep
Zhang Y.
europepmc   +1 more source

Isogeometric analysis of wing structures using multipatch parametrization and penalty-based coupling method. [PDF]

Sci Rep
Wang D, Cao X, Xue Y, Wang W, Du X.
europepmc   +1 more source