A parametric computational study of energy deposition upstream of generic two-dimensional and axisymmetric blunt bodies at Mach numbers of 6.5 and 10 is performed utilizing a full Navier-Stokes computational fluid dynamics code. The energy deposition modifies the upstream shock structure and results in large wave drag reduction and very high power effectiveness. Specifically, drag is reduced to values as low as 30% of baseline drag (no energy deposited into flow) and power effectiveness ratios (ratio of thrust power saved to power deposited into the flow) of up to 33 are obtained. The fluid dynamic and thermodynamic bases of the observed drag reduction are examined
This paper discusses the application of energy deposition for sonic boom mitigation and as actuator ...
A numerical analysis of the effects of focused energy deposition in the flow of a two-dimensional hy...
Drag force control via energy deposition in an oncoming flow is a wide area of interest in aerospace...
“A study on the use of upstream focused power deposition to reduce blunt body drag in hypersonic flo...
Numerical investigations are carried out for understanding the real gas effects for energy depositio...
This paper presents a summary and comparison of results of parametric numerical studies examining va...
We have conducted inviscid flow computations of wave drag reduction by a single pulse energy deposit...
This paper deals with the effect of electrical energy deposition on the wave drag experienced by a 1...
Energy deposition is a robust technique for various high speed flow control applications including d...
Experiments are carried out in a shock tunnel at a nominal Mach number of 5.75 in order to study the...
A series of numerical experiments were performed in which energy was deposited ahead of a cone trave...
Drag reduction technology plays a significant role in extending the flight range for a high-speed ve...
Two computational studies are performed to examine the influence of energy deposition on a blunt bod...
Effects of steady energy addition (EA) into the Mach 3 supersonic flow upstream of conically-nosed a...
We describe here an experimental study on the effect of energy deposition in the flow field of a $12...
This paper discusses the application of energy deposition for sonic boom mitigation and as actuator ...
A numerical analysis of the effects of focused energy deposition in the flow of a two-dimensional hy...
Drag force control via energy deposition in an oncoming flow is a wide area of interest in aerospace...
“A study on the use of upstream focused power deposition to reduce blunt body drag in hypersonic flo...
Numerical investigations are carried out for understanding the real gas effects for energy depositio...
This paper presents a summary and comparison of results of parametric numerical studies examining va...
We have conducted inviscid flow computations of wave drag reduction by a single pulse energy deposit...
This paper deals with the effect of electrical energy deposition on the wave drag experienced by a 1...
Energy deposition is a robust technique for various high speed flow control applications including d...
Experiments are carried out in a shock tunnel at a nominal Mach number of 5.75 in order to study the...
A series of numerical experiments were performed in which energy was deposited ahead of a cone trave...
Drag reduction technology plays a significant role in extending the flight range for a high-speed ve...
Two computational studies are performed to examine the influence of energy deposition on a blunt bod...
Effects of steady energy addition (EA) into the Mach 3 supersonic flow upstream of conically-nosed a...
We describe here an experimental study on the effect of energy deposition in the flow field of a $12...
This paper discusses the application of energy deposition for sonic boom mitigation and as actuator ...
A numerical analysis of the effects of focused energy deposition in the flow of a two-dimensional hy...
Drag force control via energy deposition in an oncoming flow is a wide area of interest in aerospace...