Add to ORKGThe interaction of on-axis and o -axis laser discharge in front of a hemisphere cylinder in Mach 2.0 ow is investigated numerically. Details of the physics of the interaction of the laser-induced shock and the heated region with the bow shock and its e ect on drag reduction are included. The energetic eciency of the laser discharge in reducing drag is calculated
There is a reinterest in hypersonic flow. There are several programs all around the world to produc...
A small-scale wind tunnel experiment has been performed to investigate the dynamics of the off-body ...
AbstractPressure sensing and schlieren imaging with high resolution and sensitivity are applied to t...
The interaction of an off-body laser discharge with a hemisphere cylinder in supersonic flow is inve...
Energy discharge is a novel method for supersonic flight control. Laser energy deposition is shown t...
Measurements of the drag over a flat-nosed cylinder with repetitive laser pulse irradiations ahead o...
A drag over a flat-nosed cylinder with repetitive laser pulse irradiations ahead of it were experime...
In this Ph.D. dissertation, two separate phenomena have been numerically studied: flow control using...
Experiments were performed within Rutgers University’s supersonic wind tunnel to investigate the eff...
Research interest has been growing in recent years in supersonic transport, particularly supersonic ...
The effects of repetitive laser-pulse energy depositions (5.5 mJ/pulse) onto a shock wave-boundary l...
Laser energy deposition provides a potential means for supersonic and hypersonic flight control wher...
Drag force control via energy deposition in an oncoming flow is a wide area of interest in aerospace...
International audienceThe goal of this study is to demonstrate experimentally the "Laser Spike" conc...
Abstract: The interaction of the laser-induced plasma produced by a pulse laser energy depo-sition w...
There is a reinterest in hypersonic flow. There are several programs all around the world to produc...
A small-scale wind tunnel experiment has been performed to investigate the dynamics of the off-body ...
AbstractPressure sensing and schlieren imaging with high resolution and sensitivity are applied to t...
The interaction of an off-body laser discharge with a hemisphere cylinder in supersonic flow is inve...
Energy discharge is a novel method for supersonic flight control. Laser energy deposition is shown t...
Measurements of the drag over a flat-nosed cylinder with repetitive laser pulse irradiations ahead o...
A drag over a flat-nosed cylinder with repetitive laser pulse irradiations ahead of it were experime...
In this Ph.D. dissertation, two separate phenomena have been numerically studied: flow control using...
Experiments were performed within Rutgers University’s supersonic wind tunnel to investigate the eff...
Research interest has been growing in recent years in supersonic transport, particularly supersonic ...
The effects of repetitive laser-pulse energy depositions (5.5 mJ/pulse) onto a shock wave-boundary l...
Laser energy deposition provides a potential means for supersonic and hypersonic flight control wher...
Drag force control via energy deposition in an oncoming flow is a wide area of interest in aerospace...
International audienceThe goal of this study is to demonstrate experimentally the "Laser Spike" conc...
Abstract: The interaction of the laser-induced plasma produced by a pulse laser energy depo-sition w...
There is a reinterest in hypersonic flow. There are several programs all around the world to produc...
A small-scale wind tunnel experiment has been performed to investigate the dynamics of the off-body ...
AbstractPressure sensing and schlieren imaging with high resolution and sensitivity are applied to t...