Add to ORKGHot-wire meassurements are made in the laminar boundary layer of a flat plate and a cone at Mach 5. These measurements do not show the expected dominance of high-frequency second-mode instabilities, predicted by linear stability theory and found in other experiments. The growth of natural disturbances within a broad frequency band up to 50 kHz on the flat plate and up to 200 kHz on the cone can be observed
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel to m...
Hot-wire measurements are made in the laminar boundary layer of a flat plate and a cone at Mach 5. T...
As part on an investigation on hypersonic boundary layer transition, first sucessful hot-wire and fl...
NOTE: text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
NOTE: text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
Studies on the stability of three-dimensional hypersonic boundary layers for 7 and 15 deg. half-angl...
Calibrated hot wires were used in the Mach-6 tunnel to obtain mass-flux profiles and to study the am...
Hypersonic boundary layer measurements were conducted over a flared cone in a quiet wind tunnel. The...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
This research experimentally investigated the effects of angle of attack, wall-to-total temperature ...
Experiments to study artificially generated disturbances in flat plate boundary layers were conducte...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel to m...
Hot-wire measurements are made in the laminar boundary layer of a flat plate and a cone at Mach 5. T...
As part on an investigation on hypersonic boundary layer transition, first sucessful hot-wire and fl...
NOTE: text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
NOTE: text or symbols not renderable in plain ASCII are indicated by [...]. Abstract is included in...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
Studies on the stability of three-dimensional hypersonic boundary layers for 7 and 15 deg. half-angl...
Calibrated hot wires were used in the Mach-6 tunnel to obtain mass-flux profiles and to study the am...
Hypersonic boundary layer measurements were conducted over a flared cone in a quiet wind tunnel. The...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
An experimental investigation of the stability of the hyper sonic laminar boundary layer was carried...
This research experimentally investigated the effects of angle of attack, wall-to-total temperature ...
Experiments to study artificially generated disturbances in flat plate boundary layers were conducte...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
In this research, to study the hypersonic boundary-layer transition, experiments were conducted on a...
Experiments have been carried out in the NASA Langley Research Center 20-Inch Mach 6 Air Tunnel to m...