The Caltech T5 reflected shock tunnel is used to produce hypervelocity flow over a range of velocities and pressures by varying the test gas and operating parameters of reservoir enthalpy (hres) and reservoir pressure (Pres). One area of research in T5 is the measurement of boundary layer behavior and transition from laminar to turbulent flow on a smooth 5-degree half-angle cone [3, 1, 11]
Experiments are carried out to address potential sources of discrepancies between experiments and si...
This experimental study documents the development and separation of a hypersonic boundary layer prod...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
The Caltech T5 reflected shock tunnel is used to produce hypervelocity flow over a range of velociti...
The Caltech T5 reflected shock tunnel is used to produce hypervelocity flow over a range of velociti...
Results are presented from an experimental exploratory study of laminar, transitional and turbulent ...
Results are presented from an experimental exploratory study of laminar, transitional and turbulent ...
Experiments to investigate the transition process in hypervelocity boundary layers were performed in...
Hypersonic boundary-layer transition on a 7 half-angle cone was investigated experimentally iin the ...
Hypersonic boundary-layer transition on a 7 half-angle cone was investigated experimentally in the D...
Recently performed linear stability analyses suggested that transition could be delayed in hypersoni...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
The laminar to turbulent transition process in boundary layer flows in thermochemical nonequilibrium...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
High speed flow visualization,wall pressure measurement and PIV were used to study the transition of...
Experiments are carried out to address potential sources of discrepancies between experiments and si...
This experimental study documents the development and separation of a hypersonic boundary layer prod...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...
The Caltech T5 reflected shock tunnel is used to produce hypervelocity flow over a range of velociti...
The Caltech T5 reflected shock tunnel is used to produce hypervelocity flow over a range of velociti...
Results are presented from an experimental exploratory study of laminar, transitional and turbulent ...
Results are presented from an experimental exploratory study of laminar, transitional and turbulent ...
Experiments to investigate the transition process in hypervelocity boundary layers were performed in...
Hypersonic boundary-layer transition on a 7 half-angle cone was investigated experimentally iin the ...
Hypersonic boundary-layer transition on a 7 half-angle cone was investigated experimentally in the D...
Recently performed linear stability analyses suggested that transition could be delayed in hypersoni...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
The laminar to turbulent transition process in boundary layer flows in thermochemical nonequilibrium...
More than 50 shots with air and 35 shots with carbon dioxide were carried out in the T5 shock tunnel...
High speed flow visualization,wall pressure measurement and PIV were used to study the transition of...
Experiments are carried out to address potential sources of discrepancies between experiments and si...
This experimental study documents the development and separation of a hypersonic boundary layer prod...
Transition from laminar to turbulent flow in hypersonic boundary layers leads to highly elevated lev...