Supersonic boundary-layer stability analysis on an aircraft wing

1991 ◽  
Vol 28 (11) ◽  
pp. 721-727 ◽  
Author(s):  
Shreekant Agrawal ◽  
Thomas A. Kinard ◽  
Arthur G. Powell
Keyword(s):  
Boundary Layer ◽  
Stability Analysis ◽  
Supersonic Boundary Layer ◽  
Boundary Layer Stability ◽  
Aircraft Wing

Influence of coating permeability and roughness on supersonic boundary layer stability

2016 ◽  
Author(s):  
V. I. Lysenko ◽  
S. A. Gaponov ◽  
B. V. Smorodsky ◽  
Yu. G. Yermolaev ◽  
A. D. Kosinov ◽  
...  
Keyword(s):  
Boundary Layer ◽  
Supersonic Boundary Layer ◽  
Boundary Layer Stability

Pre-Flight Boundary-Layer Stability Analysis of BOLT Geometry

2018 ◽  
Author(s):  
Alexander Moyes ◽  
Travis S. Kocian ◽  
Charles D. Mullen ◽  
Helen L. Reed
Keyword(s):  
Boundary Layer ◽  
Stability Analysis ◽  
Boundary Layer Stability

Influence The Direction Of Blowing Gas Through A Porous Surface On The Stability Of The Supersonic Boundary Layer

2015 ◽  
Vol 10 (2) ◽  
pp. 18-26
Author(s):  
Sergey Gaponov ◽  
Aleksandr Semenov
Keyword(s):  
Boundary Layer ◽  
Classical Method ◽  
Supersonic Boundary Layer ◽  
Porous Surface ◽  
Boundary Layer Stability ◽  
Injection Angle ◽  
Plane Plate ◽  
The Stability ◽  
Gas Blowing ◽  
Elementary Waves

In the paper the influence of the gas blowing direction through a porous surface on the supersonic boundary layer stability is investigated theoretically, using the classical method of elementary waves and the evolutionary method at Mach number M = 2. It was found that with decreasing of the gas injection angle to the plane plate the boundary layer stability was improved and the tangential blowing effect on the boundary layer stability is little in a comparison with the case of a boundary layer without mass exchange.

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