Design and computational analysis of a closed non-planar wing aircraft coupled to a boundary layer ingestion propulsion system

Author(s):  
Pedro D. Bravo Mosquera ◽  
Hernan D. Cerón-Muñoz ◽  
Fernando Catalano
Author(s):  
A Plas ◽  
D Crichton ◽  
M Sargeant ◽  
T Hynes ◽  
E Greitzer ◽  
...  

2016 ◽  
Vol 71 (9) ◽  
pp. 837-848 ◽  
Author(s):  
Ehtsham Azhar ◽  
Z. Iqbal ◽  
E.N. Maraj

AbstractThe present article dicusses the computational analysis of entropy generation for the stagnation-point flow of Sutterby nanofluid over a linear stretching plate. The Sutterby fluid is chosen to study the effect for three major classes of non-Newtonian fluids, i.e. pseudoplastic, Newtonian, and dilatant. The effects of pertinent physical parameters are examined under the approximation of boundary layer. The system of coupled nonlinear partial differential equations is simplified by incorporating suitable similarity transformation into a system of non-linear-coupled ordinary differential equations. Entropy generation analysis is conducted numerically, and the results are displayed through graphs and tables. Significant findings are listed in the closing remarks.


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