scholarly journals Pressure Distribution at the Base of a Blunt Body Due to Jet Interaction in Subsonic to Transonic Flow.

1999 ◽  
Vol 47 (547) ◽  
pp. 306-313
Author(s):  
Yoshiharu TANAHASHI ◽  
Mitsuru KURITA ◽  
Yoshiaki NAKAMURA
Author(s):  
M. H. Noorsalehi ◽  
M. Nili-Ahamadabadi ◽  
E. Shirani ◽  
M. Safari

In this study, a new inverse design method called Elastic Surface Algorithm (ESA) is developed and enhanced for axial-flow compressor blade design in subsonic and transonic flow regimes with separation. ESA is a physically based iterative inverse design method that uses a 2D flow analysis code to estimate the pressure distribution on the solid structure, i.e. airfoil, and a 2D solid beam finite element code to calculate the deflections due to the difference between the calculated and target pressure distributions. In order to enhance the ESA, the wall shear stress distribution, besides pressure distribution, is applied to deflect the shape of the airfoil. The enhanced method is validated through the inverse design of the rotor blade of the first stage of an axial-flow compressor in transonic viscous flow regime. In addition, some design examples are presented to prove the effectiveness and robustness of the method. The results of this study show that the enhanced Elastic Surface Algorithm is an effective inverse design method in flow regimes with separation and normal shock.


2020 ◽  
Vol 57 (5) ◽  
pp. 945-955
Author(s):  
Gireesh Yanamashetti ◽  
D. B. Singh ◽  
G. K. Suryanarayana ◽  
Rinku Mukherjee

2008 ◽  
Author(s):  
I. I. Salvador ◽  
M. A. S. Minucci ◽  
P. G. P. Toro ◽  
A. C. Oliveira ◽  
J. B. Channes ◽  
...  

2021 ◽  
Vol 13 (1) ◽  
Author(s):  
Ya.V. Khankhasaeva ◽  
A.L. Afendikov ◽  
A.E. Lutsky ◽  
I.S. Menshov ◽  
I.A. Znamenskaya

AIAA Journal ◽  
1969 ◽  
Vol 7 (7) ◽  
pp. 1362-1363 ◽  
Author(s):  
K. LEELAVATHI ◽  
N. R. SUBRAMANIAN

AIAA Journal ◽  
1989 ◽  
Vol 27 (9) ◽  
pp. 1301-1302 ◽  
Author(s):  
Keith Koenig ◽  
David H. Bridges ◽  
Gary T. Chapman
Keyword(s):  

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