Flow control device and method of controlling flow
The present invention relates to a flow control device and more particularly to reactive modular flow control device with deployable flow effectors. The present invention further relates to a method of operating the flow control device. One embodiment of the present invention includes a method of controlling air flow across a surface of an aircraft under certain flight conditions comprising the steps of sensing fluid separation from the surface by measuring the pressure on the surface; determining a standard deviation of the pressure measurements over a period of time; and deploying a flow of effector in response to the standard deviation of the pressure measurements exceeding a predetermined threshold number.
1. A method of controlling air flow across a surface of an aircraft under certain flight conditions comprising the steps of:
a) sensing fluid separation at a surface by measuring pressure at or near the surface;
b) calculating a standard deviation of the pressure measurements over a period of time; and
c) activating a flow control device in response to the calculated standard deviation of the pressure measurements exceeding a predetermined number.
2. The method in claim 1 , wherein the flow control device uses a vacuum or air pressure to generate a vortex at the surface.
3. The method in claim 1 , wherein the flow control device is a deployable flow effector.
4. The method in claim 2 , wherein the pressure is measured with a pressure sensor at the surface.
5. The method in claim 4 , wherein the pressure sensor and flow control device are components of a module.
6. The method in claim 3 , wherein the pressure is measured with a pressure sensor at the surface.
7. The method in claim 6 , wherein the pressure sensor and flow control device are components of a module.
8. A method for determining flow surface dynamics, comprising the steps of:
a) sensing pressure oscillation in fluid on the flow surface;
b) measuring at least one parameter of said oscillation; and
c) activating a flow control device in response to the measured parameter exceeding a predetermined limit.
9. The method of claim 8 , wherein the parameter is the amplitude of the pressure oscillation.
10. The method of claim 8 , wherein the parameter is the frequency of the pressure oscillation.
11. The method of claim 9 , wherein the parameter is the standard deviation of the amplitude of the pressure oscillation.
12. The method of claim 9 , wherein the parameter is the mean of the amplitude of the pressure oscillation.