Calculation of supersonic flow over realistic configurations by an updated low-order panel method

Author(s):  
L. FORNASIER
2012 ◽  
Vol 2012 ◽  
pp. 1-11 ◽  
Author(s):  
Ye Tian ◽  
Spyros A. Kinnas

A low order panel method is used to predict the performance of propellers. A wake alignment model based on a pseudounsteady scheme is proposed and implemented. The results from this full wake alignment (FWA) model are correlated with available experimental data, and results from RANS for some propellers at design and low advance ratios. Significant improvements have been found in the predicted integrated forces and pressure distributions.


2016 ◽  
Vol 125 ◽  
pp. 124-133 ◽  
Author(s):  
Youjiang Wang ◽  
Moustafa Abdel-Maksoud ◽  
Keqi Wang ◽  
Baowei Song

1993 ◽  
Author(s):  
ISKENDER SAHIN ◽  
JAN CRANE ◽  
KENNARD WATSON
Keyword(s):  

1978 ◽  
Author(s):  
F. EHLERS ◽  
M. EPTON ◽  
F. JOHNSON ◽  
A. MAGNUS ◽  
P. RUBBERT

1998 ◽  
Vol 25 (7) ◽  
pp. 529-539
Author(s):  
Iskender Sahin ◽  
Noriaki Okita
Keyword(s):  

AIAA Journal ◽  
1979 ◽  
Vol 17 (3) ◽  
pp. 225-226 ◽  
Author(s):  
F. E. Ehlers ◽  
M. A. Epton ◽  
F. T. Johnson ◽  
A. E. Magnus ◽  
P. E. Rubbert

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