Patent
Boundary layer control
Papst Hermann
- 16 Mar 1966
53
About: The article was published on 16 Mar 1966. The article focuses on the topics: Blasius boundary layer & Boundary layer thickness.
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Citations
Patent
Multiple-impingement cooled structure
Edward Shu-Jen Hsia,Raghuram Janaki Emani,John Howard Starkweather +2 more
- 02 Apr 1984
TL;DR: In this paper, a multiple-impingement cooled structure for turbine shroud assembly is described, which includes a plurality of baffles which define with an element to be cooled, such as a turbine shroud, with holes in one of the baffles to impinge upon only the portion of the shroud in a first cavity.
154
Patent
Laminar flow control airfoil
Louis B. Gratzer
- 24 Jul 1986
TL;DR: A laminar flow control aircraft wing combines suction surfaces and slots in its leading and trailing edge regions, with natural lamina flow over its main box region to achieve laminara boundary layer flow over a majority of the wing surface area as discussed by the authors.
89
Patent
Pneumatic aerodynamic control and drag-reduction system for ground vehicles
Robert J. Englar
- 17 Jul 1995
TL;DR: In this article, a blowing system for controlling the aerodynamics of a ground vehicle comprises a source of compressed air, a valve for regulating the flow of the compressed air and a plenum for discharging the air at a rear portion of the vehicle.
84
Numerical study of blowing and suction slot geometry optimization on NACA 0012 airfoil
TL;DR: In this article, the effects of jet width on blowing and suction flow control were evaluated for a NACA 0012 airfoil, and the results showed that when the blowing jet width increases, the lift-to-drag ratio rises continuously in tangential blowing and decreases quasi-linearly in perpendicular blowing.
Three-dimensional suction flow control and suction jet length optimization of NACA 0012 wing
Kianoosh Yousefi,Reza Saleh +1 more
TL;DR: In this article, a three-dimensional suction flow control study was performed to investigate the aerodynamic characteristics of a rectangular wing with a NACA 0012 airfoil section, and the optimum suction jet length was determined.
References
Patent
Means of reducing the fluid resistance of propelled vehicles
Edward A Stalker
- 28 Oct 1935
TL;DR: In this paper, the reduction of the fluid drag of the body by control of the boundary layer of fluid was proposed, which is related to our application of the same title, Serial No. 632,572.
57
Patent
Means for cooling machine parts
Meyer Adolf
- 09 Feb 1939
TL;DR: In this article, it has been proposed to cool turbine blades or vanes by bathing the surfaces thereof with a cooling fluid, and the distribution of the cooling fluid over the vane surfaces by delivering it through a passage in the blade from which it is discharged onto...
39
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