A 3-D CE/SE Navier-Stokes Solver with Unstructured Hexahedral Grid for Computation of Nearfield Jet Screech Noise
- Author(s):
- Publication title:
- A collection of technical papers : 9th AIAA/CEAS Aeroacoustics Conference and Exhibit, Hilton Head, South Carolina, 12-14 May 2003
- Title of ser.:
- AIAA Paper : AIAA/CEAS Aeroacoustics Conference
- Ser. no.:
- 2003
- Pub. Year:
- 2003
- Vol.:
- v. 2
- No.:
- 2003-3207
- Paper no.:
- AIAA-2003-3207
- Page(from):
- 1006
- Page(to):
- 1015
- Pages:
- 10
- Pub. info.:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563475979 [1563475979]
- Language:
- English
- Call no.:
- A07400/033100 (v.2)
- Type:
- Technical Paper
Similar Items:
1
Technical Paper
NEAR FIELD SCREECH NOISE COMPUTATION FOR AN UNDEREXPANDED SUPERSONIC JET BY THE CE/SE METHOD
American Institute of Aeronautics and Astronautics |
7
Technical Paper
Noise Computation of a Supersonic Shock-Containing Axisymmetric Jet by the CE/SE Method
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
Technical Paper
Discontinuous Galerkin Method on unstructured hexahedral grids for 3D Euler and Navier-Stokes Equations
American Institute of Aeronautics and Astronautics |
3
Technical Paper
An Implicit Spectral Difference Navier-Stokes Solver For Unstructured Hexahedral Grids
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
10
Technical Paper
An adaptive solver for the Navier-Stokes equations on unstructured hexahedral meshes
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
11
Technical Paper
Linear and Non-Validation of a Linear Multigrid Accelerated Unstructured Navier-Stokes Solver for the Computation of Turbine Blades on Hybrid Grids
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
12
Technical Paper
Three-dimensional incompressible Navier-Stokes flow computations about complete configurations using a multiblock unstructured grid approach
American Institute of Aeronautics and Astronautics |