12   Artículos

 
en línea
Ebrahim Kadivar, Mazyar Dawoodian, Yuxing Lin and Ould el Moctar    
Experimental investigations were conducted to uncover the impact of cavitation control?through the use of biomimetic riblets on cavitating flows around a circular cylinder. First, the dynamics of cavitation in the flow behind a finite cylinder (without r... ver más
Revista: Journal of Marine Science and Engineering    Formato: Electrónico

 
en línea
Peng Zhang, Rixin Cheng and Yonghong Li    
Bionic herringbone riblets are applied to relieve the flow near the blade endwall in a linear compressor cascade under the incidence angle of -4° to 6° at a Reynolds number of 382,000. The herringbone riblets are placed at the endwall upstream of the bla... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chris Bliamis, Zinon Vlahostergios, Dimitrios Misirlis and Kyros Yakinthos    
Flow control methods for aerodynamic drag reduction have been a field of interest to aircraft designers, who seek to minimize fuel consumption and increase the aircraft?s aerodynamic performance. Various flow control techniques, applied to aeronautical a... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Chaoqun Li, Shuo Tang, Yi Li and Zihai Geng    
To reduce the computational cost, the k-ω" role="presentation">??? ? SST turbulence model with Rotation and Curvature correction (SST-RC) is modified to predict the drag of practical aerodynamic configurations mounted with drag-reducing riblet... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Nils M. Barner, Luca Ghafourpour, Mustafa S. Güverte, Davide Modesti and Steven J. Hulshoff    
This work presents a transpacific airliner designed for minimal climate impact, incorporating several novel design features. These include open rotor engines, sustainable aviation fuels, natural laminar flow airfoils, and riblets. The design?s configurat... ver más
Revista: Aerospace    Formato: Electrónico

 
en línea
Hidemi Takahashi, Mitsuru Kurita, Hidetoshi Iijima and Monami Sasamori    
Turbulent boundary layer profiles on the aircraft surface were characterized by pitot-rake measurements conducted in flight experiments at high subsonic Mach number ranges. Due to slight variations in atmospheric air conditions or aircraft attitudes, suc... ver más
Revista: Applied Sciences    Formato: Electrónico

 
en línea
Jonna Tiainen, Aki Grönman, Ahti Jaatinen-Värri and Jari Backman    
The decrease in the performance of centrifugal compressors operating at low Reynolds numbers (e.g., unmanned aerial vehicles at high altitudes or small turbomachines) can reach 10% due to increased friction. The purposes of this review are to represent t... ver más

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