Apollo-Shaped Capsule Boundary Layer Transition at High-Enthalpy in T5

2010 ◽  
Author(s):  
Eric Marineau ◽  
Stuart Laurence ◽  
Hans Hornung
Keyword(s):  
Boundary Layer ◽  
Boundary Layer Transition ◽  
Layer Transition ◽  
High Enthalpy

scholarly journals Effects of Shock-Tube Cleanliness on Hypersonic Boundary Layer Transition at High Enthalpy

AIAA Journal ◽  
2017 ◽  
Vol 55 (1) ◽  
pp. 332-338 ◽  
Author(s):  
Joseph S. Jewell ◽  
Nicholaus J. Parziale ◽  
Ivett A. Leyva ◽  
Joseph E. Shepherd
Keyword(s):  
Boundary Layer ◽  
Shock Tube ◽  
Boundary Layer Transition ◽  
Hypersonic Boundary Layer ◽  
Layer Transition ◽  
High Enthalpy

scholarly journals High-Enthalpy Effects on Hypersonic Boundary-Layer Transition

2019 ◽  
Vol 56 (2) ◽  
pp. 347-356 ◽  
Author(s):  
Viola Wartemann ◽  
Alexander Wagner ◽  
Ross Wagnild ◽  
Fabio Pinna ◽  
Fernando Miró Miró ◽  
...  
Keyword(s):  
Boundary Layer ◽  
Boundary Layer Transition ◽  
Hypersonic Boundary Layer ◽  
Layer Transition ◽  
High Enthalpy

Transition of compressible high enthalpy boundary layer flow over a flat plate

1994 ◽  
Vol 98 (972) ◽  
pp. 25-34 ◽  
Author(s):  
Y. He ◽  
R. G. Morgan
Keyword(s):  
Heat Transfer ◽  
Boundary Layer ◽  
Reynolds Number ◽  
Flat Plate ◽  
Empirical Relation ◽  
Boundary Layer Transition ◽  
Transition To Turbulence ◽  
Layer Transition ◽  
High Enthalpy ◽  
Layer Flow

AbstractThis paper presents the results of an experimental investigation into the characteristics of boundary layer transition to turbulence in hypervelocity air flows. A series of experiments was conducted using a flat plate model, equipped with static pressure and thin film heat transfer transducers, in a free piston shock tunnel. Transition was observed in the stagnation enthalpy range of 2·35 to 19·2 MJ/kg. The transition Reynolds number correlates well with the unit Reynolds number through a simple empirical relation. The influences of Mach number, pressure and wall cooling are examined. The measured heat transfer rates in laminar and turbulent regions are compared with empirical predictions. Freestream disturbances of the test flow were also measured and analysed.

Sign in / Sign up

Export Citation Format

Share Document