Claims
- 1. A method for reducing skin friction, inhibiting the effects of liquid turbulence, and decreasing heat transfer between a contact area of a body surface and a liquid flow, comprising the steps of:
- providing adjacent, longitudinal grooves in the body surface along the entire contact area of the body surface; and
- injecting an individual gas stream into each groove; wherein each longitudinal groove is sized to trap the respective individual stream; whereby an array of gas tubes are formed between the grooves and the liquid flow.
- 2. The method according to claim 1, further comprising applying a surfactant to the adjacent longitudinal groove, the surfactant having a thickness and roughness which allows the injected gas streams to be trapped within the grooves at increased gas velocities.
- 3. The method according to claim 1, wherein the gas is injected into each groove at a downstream angle of approximately 45.degree..
- 4. The method according to claim 3, wherein the gas is injected into a valley of each groove.
- 5. The method according to claim 1, wherein the gas is injected at a velocity which is a substantial portion of the velocity of the liquid flow.
- 6. A mechanism for reducing skin friction between a liquid flow and a contact area of a body surface comprising:
- adjacent, longitudinal grooves formed in the body surface along the entire contact area;
- means for injecting individual gas streams downstream into each of said adjacent, longitudinal grooves, wherein each of said grooves is sized to trap the respective individual gas stream, whereby an array of tubes of gas are formed between the grooves and the liquid flow.
- 7. The mechanism according to claim 6, wherein a surfactant is applied to said grooves to further reduce the friction between the liquid flow and the contact area, the surfactant having a thickness and roughness which allows the injected gas streams to be trapped within said grooves.
- 8. The mechanism according to claim 6, wherein said injecting means injects the gas streams at an angle of 45.degree. relative to the contact area.
- 9. The mechanism according to claim 8, wherein said injecting means injects the gas streams into a valley of each groove.
- 10. The mechanism according to claim 6, wherein said grooves are triangular.
- 11. The mechanism according to claim 10, wherein the triangular grooves are arranged such that minimal contact occurs between the liquid and the contact area.
- 12. The mechanism according to claim 6, wherein said injecting means injects the gas streams at a velocity which is a substantial portion of the velocity of a liquid flow.
ORIGIN OF THE INVENTION
The invention described herein was made jointly in the performance of work under a NASA Contract and by an employee of the United States Government. In accordance with 35 USC 202, the contractor elected not to retain title.
US Referenced Citations (10)
Foreign Referenced Citations (2)
Number |
Date |
Country |
752117 |
Jul 1980 |
SUX |
1300132 |
Dec 1972 |
GBX |