Turbulence Production and Transport in Quasi-Two-Dimensional Wake/Boundary-Layer Interaction

AIAA Journal ◽  
10.2514/2.980 ◽  
2000 ◽  
Vol 38 (2) ◽  
pp. 259-265 ◽  
Author(s):  
G. A. Sideridis ◽  
E. G. Kastrinakis ◽  
S. G. Nychas
Keyword(s):  
Boundary Layer ◽  
Two Dimensional ◽  
Layer Interaction ◽  
Boundary Layer Interaction ◽  
Turbulence Production

Turbulence production and transport in quasi-two-dimensional wake/boundary-layer interaction

AIAA Journal ◽  
2000 ◽  
Vol 38 ◽  
pp. 259-265
Author(s):  
G. A. Sideridis ◽  
E. G. Kastrinakis ◽  
S. G. Nychas
Keyword(s):  
Boundary Layer ◽  
Two Dimensional ◽  
Layer Interaction ◽  
Boundary Layer Interaction ◽  
Turbulence Production

Effect of Shock Boundary Layer Interaction on Aerofoil Pressure Distributions at Transonic Speeds

1963 ◽  
Vol 67 (634) ◽  
pp. 674-677
Author(s):  
D. Tirumalesa
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Turbulent Boundary Layer ◽  
Two Dimensional ◽  
Relative Thickness ◽  
Circular Arc ◽  
Layer Interaction ◽  
Pressure Distributions ◽  
Boundary Layer Interaction ◽  
Theoretical Results

SummaryA method of improving pressure distributions predicted by inviscid theory over two-dimensional aerofoils at transonic speeds taking into account shock-wave turbulent boundary layer interaction as obtained in the case of the flat plate is described.The method was applied to a non-lifting circular arc aerofoil of eight per cent relative thickness. The shock wave location, pressure distribution and drag coefficient were calculated and compared with experimental and inviscid theoretical results.It has been found that the method gives results which are consistent with experimental results in various aspects.

scholarly journals CFD Validation Experiment of a Mach 2.5 Axisymmetric Shock-Wave/Boundary-Layer Interaction

2015 ◽  
Author(s):  
David O. Davis
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Region Of Interest ◽  
Two Dimensional ◽  
Cfd Validation ◽  
Layer Interaction ◽  
Wave Boundary Layer ◽  
Validation Experiment ◽  
Boundary Layer Interaction ◽  
Wave Boundary

Preliminary results of an experimental investigation of a Mach 2.5 two-dimensional axisymmetric shock-wave/boundary-layer interaction (SWBLI) are presented. The purpose of the investigation is to create a SWBLI dataset specifically for CFD validation purposes. Presented herein are the details of the facility and preliminary measurements characterizing the facility and interaction region. These results will serve to define the region of interest where more detailed mean and turbulence measurements will be made.

Two-Dimensional Shock-Wave/Boundary-Layer Interaction in the Presence of Entropy Layer

AIAA Journal ◽  
2013 ◽  
Vol 51 (1) ◽  
pp. 80-93 ◽  
Author(s):  
Volf Y. Borovoy ◽  
Ivan V. Egorov ◽  
Arkady S. Skuratov ◽  
Irina V. Struminskaya
Keyword(s):  
Boundary Layer ◽  
Shock Wave ◽  
Two Dimensional ◽  
Entropy Layer ◽  
Layer Interaction ◽  
Wave Boundary Layer ◽  
Boundary Layer Interaction ◽  
Wave Boundary

Control of Incident Shock/Boundary-Layer Interaction by a Two-Dimensional Bump

AIAA Journal ◽  
2014 ◽  
Vol 52 (4) ◽  
pp. 767-776 ◽  
Author(s):  
Yue Zhang ◽  
Hui-jun Tan ◽  
Fang-Chao Tian ◽  
Yi Zhuang
Keyword(s):  
Boundary Layer ◽  
Incident Shock ◽  
Two Dimensional ◽  
Layer Interaction ◽  
Shock Boundary Layer Interaction ◽  
Boundary Layer Interaction
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