Javascript must be enabled to continue!
Influence of laser-generated perturbations on hypersonic boundary-layer stability
View through CrossRef
In this paper, the boundary layer flow stability is investigated experimentally in a 7° half-angle straight cone under the condition of Mach number 6 and unit Reynolds number 3.1×106/m. Expanded shock wave generated by focusing laser in a limit space is used as the small artificial disturbance, and the influence of the laser-generated perturbation on the stability of the hypersonic boundary layer is analyzed. In the experiment, the wall fluctuation pressure is measured by the high-frequency pressure sensors whose response frequencies each reach a value on the order of megahertz. Through the short time Fourier transformation and power spectrum density analysis of the pressure data, the results show that when the laser-generated perturbation is added to the flow field, the position of the second mode wave advances and the amplitude of the disturbance wave greatly increases. Within the same flow range, the laser focusing on disturbance pushes the disturbance wave in the boundary layer from the linear development phase into the nonlinear development state. The laser-generated perturbation has a significant effect on the promotion of the development of disturbance waves in the boundary layer. At the same time, laser-generated perturbation that has different influences on the boundary layer when it focuses on different positions. When the laser focus disturbance focuses on the location X=100 mm, the amplitude of the disturbance wave with a frequency of 90 kHz in the boundary layer grows fastest, and the amplitude magnification at the position of X=500 mm is 3.81. When the laser perturbation is added to the free flow in front of the cone, the frequency of the disturbance wave with the fastest amplitude increase speed greatly decreases to 73 kHz. In the same range, the amplitude magnification is 4.51 times. It can be seen that when the laser focuses on the free stream upstream from the cone, its effect on the disturbance wave in the boundary layer is more significant.
Acta Physica Sinica, Chinese Physical Society and Institute of Physics, Chinese Academy of Sciences
Title: Influence of laser-generated perturbations on hypersonic boundary-layer stability
Description:
In this paper, the boundary layer flow stability is investigated experimentally in a 7° half-angle straight cone under the condition of Mach number 6 and unit Reynolds number 3.
1×106/m.
Expanded shock wave generated by focusing laser in a limit space is used as the small artificial disturbance, and the influence of the laser-generated perturbation on the stability of the hypersonic boundary layer is analyzed.
In the experiment, the wall fluctuation pressure is measured by the high-frequency pressure sensors whose response frequencies each reach a value on the order of megahertz.
Through the short time Fourier transformation and power spectrum density analysis of the pressure data, the results show that when the laser-generated perturbation is added to the flow field, the position of the second mode wave advances and the amplitude of the disturbance wave greatly increases.
Within the same flow range, the laser focusing on disturbance pushes the disturbance wave in the boundary layer from the linear development phase into the nonlinear development state.
The laser-generated perturbation has a significant effect on the promotion of the development of disturbance waves in the boundary layer.
At the same time, laser-generated perturbation that has different influences on the boundary layer when it focuses on different positions.
When the laser focus disturbance focuses on the location X=100 mm, the amplitude of the disturbance wave with a frequency of 90 kHz in the boundary layer grows fastest, and the amplitude magnification at the position of X=500 mm is 3.
81.
When the laser perturbation is added to the free flow in front of the cone, the frequency of the disturbance wave with the fastest amplitude increase speed greatly decreases to 73 kHz.
In the same range, the amplitude magnification is 4.
51 times.
It can be seen that when the laser focuses on the free stream upstream from the cone, its effect on the disturbance wave in the boundary layer is more significant.
Related Results
Stability characteristic of hypersonic flow over a blunt wedge under freestream pulse wave
Stability characteristic of hypersonic flow over a blunt wedge under freestream pulse wave
AbstractTo investigate the stability characteristic of hypersonic flow under the action of a freestream pulse wave, a high-order finite difference method was employed to do directi...
LEO-to-GNSS Laser Interferometer for Space Geodesy with Laser DORIS and Laser SAR
LEO-to-GNSS Laser Interferometer for Space Geodesy with Laser DORIS and Laser SAR
In order to increase the accuracy of precise orbit determination for a single satellite or satellites in LEO formation, we propose using a LEO-to-GNSS laser interferometer, what we...
Laser Spectrometric Techniques in Analytical Atomic Spectrometry
Laser Spectrometric Techniques in Analytical Atomic Spectrometry
Abstract
Laser light has a number of spectacular properties that make it useful for analytical spectrometry. One is that it has a high directionality (i.e. i...
EVALUATING THE IMPACT OF SURFACE TRANSVERSE CURVATURE ON BOUNDARY LAYER FLOWS: AN EXTENDED THWAITES INTEGRAL APPROACH
EVALUATING THE IMPACT OF SURFACE TRANSVERSE CURVATURE ON BOUNDARY LAYER FLOWS: AN EXTENDED THWAITES INTEGRAL APPROACH
The existing Thwaites integral method does not account for the surface transverse curvature (TVC) effects on laminar boundary layer flows over axisymmetric bodies of revolution. Mo...
Impact des perturbations sur les communautés végétales des écosystèmes prairiaux de moyenne montagne
Impact des perturbations sur les communautés végétales des écosystèmes prairiaux de moyenne montagne
En Europe, les prairies semi-naturelles de moyenne montagne sont principalement des écosystèmes ayant évolués au cours de plusieurs décennies d’activité humaine. Ces écosystèmes pr...
Transitional periods of the atmospheric boundary layer
Transitional periods of the atmospheric boundary layer
The atmospheric boundary layer is the part of the troposphere influenced by the presence of the surface, and where most weather phenomena occur. During the day, with fair weather c...
Electromagnetic scattering characteristics of foil in hypersonic plasma turbulence
Electromagnetic scattering characteristics of foil in hypersonic plasma turbulence
To investigate the electromagnetic scattering problem related to a foil in a turbulent hypersonic plasma environment, the scattering field formulas for hypersonic plasma turbulence...
Beyond the Atmosphere: The Revolution in Hypersonic Flight
Beyond the Atmosphere: The Revolution in Hypersonic Flight
Hypersonic flight, defined as traveling at speeds greater than Mach 5, represents a revolutionary frontier in aerospace technology, promising transformative impacts on both militar...

