Turbulent spots in boundary layers in a free-piston shock-tunnel flow

Shock Waves ◽  
1996 ◽  
Vol 6 (6) ◽  
pp. 337-343 ◽  
Author(s):  
D. J. Mee ◽  
C. P. Goyne
Keyword(s):  
Boundary Layers ◽  
Shock Tunnel ◽  
Free Piston ◽  
Turbulent Spots

Turbulent spots in boundary layers in a free-piston shock-tunnel flow

Shock Waves ◽  
1996 ◽  
Vol 6 (6) ◽  
pp. 337-1
Author(s):  
D.J. Mee ◽  
C.P. Goyne
Keyword(s):  
Boundary Layers ◽  
Shock Tunnel ◽  
Free Piston ◽  
Turbulent Spots

Free-flight measurement technique in the free-piston high-enthalpy shock tunnel

2014 ◽  
Vol 85 (4) ◽  
pp. 045112 ◽  
Author(s):  
H. Tanno ◽  
T. Komuro ◽  
K. Sato ◽  
K. Fujita ◽  
S. J. Laurence
Keyword(s):  
Measurement Technique ◽  
Shock Tunnel ◽  
Free Flight ◽  
Free Piston ◽  
High Enthalpy ◽  
Flight Measurement ◽  
High Enthalpy Shock Tunnel

Preliminary results with a free piston shock tunnel

AIAA Journal ◽  
1965 ◽  
Vol 3 (6) ◽  
pp. 1170-1171 ◽  
Author(s):  
R. J. STALKER
Keyword(s):  
Shock Tunnel ◽  
Free Piston ◽  
Preliminary Results

Design and Characterization of the Sandia Free-Piston Reflected Shock Tunnel

2022 ◽  
Author(s):  
Kyle P. Lynch ◽  
Thomas Grasser ◽  
Paul Farias ◽  
Kyle Daniel ◽  
Russell Spillers ◽  
...  
Keyword(s):  
Shock Tunnel ◽  
Free Piston ◽  
Reflected Shock

One-Dimensional Simulation of Free-Piston Shock Tunnel/Expansion Tubes

1995 ◽  
pp. 457-462
Author(s):  
M. Mitsuda ◽  
T. Oda ◽  
T. Kurosaka ◽  
S. Wakuri ◽  
T. Arai
Keyword(s):  
Shock Tunnel ◽  
Free Piston ◽  
One Dimensional ◽  
Dimensional Simulation ◽  
Expansion Tubes

Initial Testing of a 2 m Mach-10 Free-Piston Shock Tunnel

2019 ◽  
pp. 213-219
Author(s):  
Junmou Shen ◽  
Handong Ma ◽  
Chen Li ◽  
Xing Chen ◽  
Bi Zhixian
Keyword(s):  
Shock Tunnel ◽  
Free Piston ◽  
Initial Testing ◽  
Mach 10

Investigation of the Laminar-Turbulent Transition of Boundary Layers Disturbed by Wakes

1982 ◽  
Author(s):  
H. Pfeil ◽  
R. Herbst ◽  
T. Schröder
Keyword(s):  
Boundary Layer ◽  
Pressure Gradient ◽  
Boundary Layers ◽  
Transition Process ◽  
Boundary Layer Transition ◽  
Layer Transition ◽  
Turbulent Spots ◽  
Turbulent Transition ◽  
Time Space ◽  
Favorable Pressure Gradient

The boundary layer transition under instationary afflux conditions as present in the stages of turbomachines is investigated. A model for the transition process is introduced by means of time-space distributions of the turbulent spots during transition and schematic drawings of the instantaneous boundary layer thicknesses. To confirm this model, measurements of the transition with zero and favorable pressure gradient are performed.

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