IP Library Granted Patent US 8,935,140
Granted Patent B2
US 8,935,140 · App. 13/887,189 · Granted Jan 13, 2015

Generating inviscid and viscous fluid-flow simulations over a surface using a fluid-flow mesh

Inventors: David L. Rodriguez (Palo Alto, CA); Peter Sturdza (Redwood City, CA)
Assignee: Aerion Corporation
G06F17/5009G06F17/5018G06F17/5095G06F17/18G06F19/704G06F2217/16G06F2217/46
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Quick Facts
Patent No.
US 8,935,140
App. No.
13/887,189
Granted
Jan 13, 2015
Kind
B2
Abstract

Fluid-flow simulation over a computer-generated surface is generated using inviscid and viscous simulations. A fluid-flow mesh of fluid cells is obtained. At least one inviscid fluid property for the fluid cells is determined using an inviscid fluid simulation that does not simulate fluid viscous effects. A set of intersecting fluid cells that intersects the surface are identified. A surface mesh polygon of the surface mesh is identified for each intersecting fluid cell. At least one boundary-layer fluid property for each identified surface mesh polygon is determined using the at least one inviscid fluid property of the corresponding intersecting fluid cell and a boundary-layer simulation that simulates fluid viscous effects.

Claims (46)

1. A computer-implemented method of generating a fluid-flow simulation over a computer-generated surface, the computer-generated surface comprised of a surface mesh of surface mesh polygons, the method comprising:

obtaining a fluid-flow mesh for simulating a fluid flow over the surface, the fluid-flow mesh comprising a plurality of fluid cells;

determining at least one inviscid fluid property for each of the fluid cells using an inviscid fluid simulation that does not simulate fluid viscous effects;

identifying a set of intersecting fluid cells of the plurality of fluid cells, wherein the set of intersecting fluid cells intersects the surface;

identifying a set of surface mesh polygons of the surface mesh, wherein each surface mesh polygon of the set of surface mesh polygons corresponds to an intersecting fluid cell of the set of intersecting fluid cells, and wherein a number of surface mesh polygons of set of surface mesh polygons is fewer than a total number of surface mesh polygons that are intersected by the set of intersecting fluid cells;

determining at least one boundary-layer fluid property for at least one identified surface mesh polygon using the at least one inviscid fluid property of the corresponding intersecting fluid cell and a boundary-layer simulation that simulates fluid viscous effects.

2. The computer-implemented method of claim 1 , further comprising:

determining at least one updated fluid property for the intersecting fluid cell of the set of intersecting fluid cells using the at least one boundary-layer fluid property and the inviscid fluid simulation.

3. The computer-implemented method of claim 1 , wherein identifying the set of surface mesh polygons comprises:

obtaining a centroid of the intersecting fluid cell of the set of intersecting fluid cells;

identifying a surface mesh polygon having a centroid that is closest to the centroid of the intersecting fluid cell.

4. The computer-implemented method of claim 3 , wherein the centroid of the intersecting fluid cell is the centroid of a region of the intersecting fluid cell that is outside of the surface.

5. The computer-implemented method of claim 1 , wherein the at least one boundary-layer fluid property includes a boundary-layer thickness value, the boundary-layer thickness value representing a distance from the surface where fluid viscous effects can be ignored.

6. The computer-implemented method of claim 1 , wherein the at least one boundary-layer fluid property includes a transpiration flux value, the transpiration flux value representing a direction and an amount of fluid flow originating from the surface.

7. The computer-implemented method of claim 1 , wherein the inviscid fluid simulation is an Euler-based flow simulation.

8. The computer-implemented method of claim 1 , wherein the at least one inviscid fluid property includes a fluid velocity vector, a fluid density value, and a fluid pressure value.

9. The computer-implemented method of claim 1 , wherein the computer-generated surface is an aircraft surface.

10. A computer-implemented method of generating a fluid-flow simulation over a computer-generated surface, the computer-generated surface comprised of a surface mesh of surface mesh polygons, the method comprising:

obtaining a fluid-flow mesh for simulating a fluid flow over the surface, the fluid-flow mesh comprising a plurality of fluid cells;

determining at least one inviscid fluid property for each of the fluid cells using an inviscid fluid simulation that does not simulate fluid viscous effects;

identifying an intersecting fluid cell of the plurality of fluid cells that intersects the surface;

determining a single boundary-layer prediction point for the intersecting fluid cell resulting in a one-to-one correlation between the intersecting fluid cell and the boundary-layer prediction point; and

determining at least one boundary-layer fluid property for the boundary-layer prediction point using the at least one inviscid fluid property of the intersecting fluid cell.

11. A non-transitory computer-readable storage medium comprising computer-executable instructions for generating a fluid-flow simulation over a computer-generated surface, the computer-generated surface comprised of a surface mesh of surface mesh polygons, the instructions for:

obtaining a fluid-flow mesh for simulating a fluid flow over the surface, the fluid-flow mesh comprising a plurality of fluid cells;

determining at least one inviscid fluid property for each of the fluid cells using an inviscid fluid simulation that does not simulate fluid viscous effects;

identifying a set of intersecting fluid cells of the plurality of fluid cells, wherein the set of intersecting fluid cells intersects the surface;

identifying a set of surface mesh polygons of the surface mesh, wherein each surface mesh polygon of the set of surface mesh polygons corresponds to an intersecting fluid cell of the set of intersecting fluid cells, and wherein a number of surface mesh polygons of set of surface mesh polygons is fewer than a total number of surface mesh polygons that are intersected by the set of intersecting fluid cells; and

determining at least one boundary-layer fluid property for at least one identified surface mesh polygon using the at least one inviscid fluid property of the corresponding intersecting fluid cell and a boundary-layer simulation that simulates fluid viscous effects.

12. The computer-readable storage medium of claim 11 , the instructions further comprising:

determining at least one updated fluid property for the intersecting fluid cell of the set of intersecting fluid cells using the at least one boundary-layer fluid property and the inviscid fluid simulation.

13. The computer-readable storage medium of claim 11 , wherein identifying the set of surface mesh polygons comprises instructions for:

obtaining a centroid of the intersecting fluid cell of the set of intersecting fluid cells;

identifying a surface mesh polygon having a centroid that is closest to the centroid of the intersecting fluid cell.

14. The computer-readable storage medium of claim 13 , wherein the centroid of the intersecting fluid cell is the centroid of a region of the intersecting fluid cell that is outside of the surface.

15. The computer-readable storage medium of claim 11 , wherein the at least one boundary-layer fluid property includes a boundary-layer thickness value, the boundary-layer thickness value representing a distance from the surface where fluid viscous effects can be ignored.

16. The computer-readable storage medium of claim 11 , wherein the at least one boundary-layer fluid property includes a transpiration flux value, the transpiration flux value representing a direction and an amount of fluid flow originating from the surface.

17. The computer-readable storage medium of claim 11 , wherein the inviscid fluid simulation is an Euler-based flow simulation.

18. The computer-readable storage medium of claim 11 , wherein the at least one inviscid fluid property includes a fluid velocity vector, a fluid density value, and a fluid pressure value.

19. The computer-readable storage medium of claim 11 , wherein the computer-generated surface is an aircraft surface.

20. A non-transitory computer-readable storage medium comprising computer-executable instructions for generating a fluid-flow simulation over a computer-generated surface, the computer-generated surface comprised of a surface mesh of surface mesh polygons, the instructions comprising instructions for:

obtaining a fluid-flow mesh for simulating a fluid flow over the surface, the fluid-flow mesh comprising a plurality of fluid cells;

determining at least one inviscid fluid property for each of the fluid cells using an inviscid fluid simulation that does not simulate fluid viscous effects;

identifying an intersecting fluid cell of the plurality of fluid cells that intersects the surface;

determining a single boundary-layer prediction point for the intersecting fluid cell resulting in a one-to-one correlation between the intersecting fluid cell and the boundary-layer prediction point; and

determining at least one boundary-layer fluid property for the boundary-layer prediction point using the at least one inviscid fluid property of the intersecting fluid cell.

Assignments (6)
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 21, 2023
From: LUZINSKI, JOSEPH J
To: BOEING ACE COLLATERAL AGENT, LLC
Reel/Frame 063710/0928 →
SECURITY INTEREST Recorded Jul 12, 2021
From: AERION CORPORATION; AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
To: BOEING ACE COLLATERAL AGENT LLC, AS COLLATERAL AGENT
Reel/Frame 056819/0235 →
SECURITY INTEREST Recorded Mar 25, 2021
From: AERION CORPORATION; AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
To: BOEING ACE COLLATERAL AGENT LLC, AS COLLATERAL AGENT
Reel/Frame 055724/0653 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jan 15, 2019
From: AERION CORPORATION
To: AERION INTELLECTUAL PROPERTY MANAGEMENT CORPORATION
Reel/Frame 048077/0026 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 21, 2014
From: DESKTOP AERONAUTICS, INC.
To: AERION CORPORATION
Reel/Frame 034236/0284 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Nov 20, 2014
From: RODRIGUEZ, DAVID L.; STURDZA, PETER
To: DESKTOP AERONAUTICS, INC.
Reel/Frame 034224/0832 →
Continuity (2)
Continuation 12982744 · Dec 30, 2010
Related Publication 20130246027A1 · Sep 19, 2013