A New Characteristic Nonreflecting Boundary Condition for the Multidimensional Navier-Stokes Equations

A New Characteristic Nonreflecting Boundary Condition for the Multidimensional Navier-Stokes Equations

Author(s):

Yaguchi, T. ( University of Tokyo, Bunkyo-ku, Japan )
Sugihara, K.

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA/CEAS Aeroacoustics Conference

Ser. no.:

11th

Pub. Year:

2005

No.:

2005-2868

Paper no.:

AIAA Paper 2005-2868

Pub. info.:

[Reston, Va.]: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200510 [CD-ROM 2005 Disc 10]

Type:

Technical Paper

Details

TDL ID:	ZA00001625
Series ID:	PA00000149
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference ; AIAA Aeroacoustics Conference
Conf. info. (Number):	11th ; 26th
Conf. info. (Venue):	Monterey, California
Conf. info. (Date):	2005.05.23-2005.05.25

Similar Items:

1 Technical Paper CHARACTERISTICS AND BOUNDARY ELEMENTS FOR THREE DIMENSIONAL NONSTATIONARY NAVIER STOKES FLOWS HEBEKER, F.-K. National Aeronautics and Space Administration	7 Technical Paper Numerical Validation of Characteristic and Linearized Unsteady Boundary Conditions for Non-Integer Blade Ratios in a Non-Linear Navier Stokes Solver. Mokulys, T., Dewhurst, S.C., Abhari, R.S. American Society of Mechanical Engineers
2 Technical Paper SSME THRUST CHAMBER SIMULATION USING NAVIER STOKES EQUATIONS Przekwas, A. J., Singhal, A. K., Tam, L. T. National Aeronautics and Space Administration	8 Technical Paper A new scheme for the incompressible navier-stokes equations employing alternating-direction operator splitting and domain decomposition Spyropoulos, John T., Douglas, Jim, Jr., Lyrintzis, A.S. American Institute of Aeronautics and Astronautics
3 Technical Paper An O(Nm2)Plane Solver for the Compressible Navier-Stokes Equations Thomas, J. L., Bonhaus, D. L., Anderson, W. K., Rumsey, C. L., Biedron, R. T. American Institute of Aeronautics and Astronautics	9 Technical Paper Three-Dimensional Navier-Stokes Simulations with Two-Equation Turbulence Models of Intersecting Shock-Waves/Turbulent Boundary Layer at Mach 8.3 Bardina, J. E., Coakley, T. J. National Aeronautics and Space Adminstration
4 Technical Paper An O(Nm2) plane solver for the compressible Navier-Stokes equations Thomas, J.L., Bonhaus, D.L., Anderson, W.K., Rumsey, C.L., Biedron, R.T. American Institute of Aeronautics and Astronautics	10 Technical Paper Numerically nonreflecting boundary conditions for multidimensional aeroacoustic computations Rowley, Clarence W., Colonius, Tim American Institute of Aeronautics and Astronautics
5 Technical Paper Intermittency Based Unsteady Boundary Layer Transition Modeling, Implementation into Navier- Stokes Equations. Schobeiri, M.T. American Society of Mechanical Engineers	11 Technical Paper BOUNDDARY CONDITIONS FOR THE NAVIER-STOKE'S EQUATIONS AT AN ARTIFICIAL BOUNDARY INTERSECTING A SOLID BOUNDARY Gustafsson, Bertil, Nordstroem, Jan National Aeronautics and Space Adminstration
6 Technical Paper STUDY OF FLOW PAST A CIRCULAR CYLINDER USING A HIGHER ORDER SCHEME FOR NAVIER-STOKES EQUATION Sengupta, T. K. et al. National Aeronautics and Space Administration	12 Technical Paper Lebesque Measures for Transient Response of the Navier-Stokes Equations Bobba, K. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12