scholarly journals Numerical analysis of the influence of the front heat shield separation process from the descent module on their aerodynamic characteristics

2020 ◽  
Vol 1705 ◽  
pp. 012029
Author(s):  
V.T. Kalugin ◽  
A.Yu. Lutsenko ◽  
D.M. Slobodyanuk
2018 ◽  
Vol 148 ◽  
pp. 153-162 ◽  
Author(s):  
Nikolay A. Elisov ◽  
Sergey A. Ishkov ◽  
Valentin G. Shakhov

Author(s):  
F. Etemadi ◽  
M. Mani ◽  
M. Etemadi

This article investigates the aerodynamic characteristics of repairing the airfoil with triangular damage by the measurement of aerodynamic coefficients improvement. For study of this model “two applied and numerical methods are used”. A full span NACA 641-412 airfoil is considered as test model. Using model is in five schematics: undamaged model, damaged model with upper, lower and full repair model. The used repair sheets are chosen based on the ABDR manuals. Effect of the repair on different shape of damage has performed by the quantity and quality results.


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