Acceso al sitio web del Consejo de Políticas de Infraestructura

   
Redirigiendo al acceso original de articulo en 18 segundos...
ARTÍCULO
TITULO

Boundary Layer Stability Regime at DACCIWA Site Using Gradient Richardson Number

O. O. Ajileye    
M. A. Ayoola    

Resumen

No disponible

PÁGINAS
pp. Page:402 - 415Abstrac

 Artículos similares

       
 
Ranran Huang, Tao Xue and Jie Wu    
A two-point cylindrical-focused laser differential interferometer (2P-CFLDI) system and a conventional Z-type Schlieren were used to measure the hypersonic turbulent boundary layer on a flat plate at Mach number Ma = 6 and Reynolds number Re = 1.08 × 106... ver más
Revista: Aerospace

 
Aristia L. Philippou, Pavlos K. Zachos and David G. MacManus    
High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow instability known as ?buzz?, characterized by unsteady shock oscillations at the inlet. This paper presents a comprehensive review of prior research, focused on un... ver más
Revista: Aerospace

 
Yanxin Yin, Ruiyang Lu, Jianxin Liu and Zhangfeng Huang    
Temperatures within the boundary layers of high-enthalpy hypersonic flows can soar to thousands or even tens of thousands of degrees, leading to significant real gas phenomena. Although there has been significant research on real gas effects on hypersoni... ver más
Revista: Aerospace

 
Ming Qi, Wenguo Zhu and Shu Li    
The flight of a migratory bird-like flapping-wing aircraft is characterized by a low Reynolds number and unsteadiness. The selection of airfoil profiles is critical to designing an efficient flapping-wing aircraft. To choose the suitable airfoil for vari... ver más
Revista: Aerospace

 
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