U.S. patents available from 1976 to present.
U.S. patent applications available from 2005 to present.

Surface for low drag in turbulent flow

Patent 5114099 Issued on May 19, 1992. Estimated Expiration Date: Icon_subject June 4, 2010. Estimated Expiration Date is calculated based on simple USPTO term provisions. It does not account for terminal disclaimers, term adjustments, failure to pay maintenance fees, or other factors which might affect the term of a patent.

Patent References

1454479

1726882

2608171

2800291

2899150

3184184

3213819

Driven craft having surface means for increasing propulsion efficiencies
Patent #: 4284302
Issued on: 08/18/1981
Inventor: Drews

Airstream modification device for airfoils
Patent #: 4354648
Issued on: 10/19/1982
Inventor: Schenk ,   et al.

Low drag surface
Patent #: 4434957
Issued on: 03/06/1984
Inventor: Moritz

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Inventor

Assignee

Application

No. 532864 filed on 06/04/1990

US Classes:

244/130, Aerodynamic resistance reducing244/200By characteristic of airfoil's skin

Examiners

Primary: Peters, Joseph F. Jr.
Assistant: Mattix, Carla

Attorney, Agent or Firm

Foreign Patent References

  • 3609541 DE 09/12/1987

International Class

B64C 021/10

Abstract

A nonsmooth surface of an object in a fluid flowstream permits a reduction of turbulent drag. The surface shape is designed to approximate a minimal surface and satisfies the equation (V⋅∇)∇Φ=0, where V is the relative velocity between the fluid and the surface, ∇Φ is the velocity of the strain tensor. The improved surface shape may be an array of diamond shaped elements having an airfoil like diagonal along the streamline, or it may be a series of wavelets juxtaposed to one another. The specific shape of the various types of elements to be used on the surface is selected based upon the acceleration or deceleration of the fluid at the particular position on the surface, as well as the intensity of the turbulence at that position.

Other References

  • NASA Tech Briefs, Summer 1980, "Grooves Reduce Aircraft Drag," M. J. Walsh, Langley Research Center, p. 192
  • Gao, Ge, "On Perturbation Equation of Navier-Stokes Equation", Journal of Aerospace Power, vol. 4, No. 2, pp. 189-192 (Apr. 1989
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