Stability and Receptivity of the Swept-Wing Boundary-Layer Flow Controlled by a Periodic Sequence of Plasma Actuators

2021 ◽  
Vol 56 (5) ◽  
pp. 630-644
Author(s):  
S. V. Manuilovich
1967 ◽  
Vol 18 (2) ◽  
pp. 150-164 ◽  
Author(s):  
N. A. Cumpsty ◽  
M. R. Head

SummaryAn earlier paper described a method of calculating the turbulent boundary layer flow over the rear of an infinite swept wing. It made use of an entrainment equation and momentum integral equations in streamwise and cross-flow directions, together with several auxiliary assumptions. Here the method is adapted to the calculation of the turbulent boundary layer flow along the attachment line of an infinite swept wing. In this case the cross-flow momentum integral equation reduces to the identity 0 = 0 and must be replaced by its differentiated form. Two alternative approaches are also adopted and give very similar results, in good agreement with the limited experimental data available. It is found that results can be expressed as functions of a single parameter C*, which is evidently the criterion of similarity for attachment-line flows.


2015 ◽  
Vol 46 (8) ◽  
pp. 733-752
Author(s):  
Marat Dzhaudatovich Gamirullin ◽  
Alexander Petrovich Kuryachii ◽  
Vladimir Mikhailovich Litvinov ◽  
Aleksandr Aleksandrovich Uspenskii ◽  
Sergei Leonidovich Chernyshev

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