NEAR FIELD SCREECH NOISE COMPUTATION FOR AN UNDEREXPANDED SUPERSONIC JET BY THE CE/SE METHOD

NEAR FIELD SCREECH NOISE COMPUTATION FOR AN UNDEREXPANDED SUPERSONIC JET BY THE CE/SE METHOD

Author(s):

Loh,Ching Y. ( Taitech Inc. )
Hultgren,Lennart S. ( NASA Glenn Research Center )
Jorgenson,Philip C.E.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Atmospheric Flight Mechanics Conference

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-2252

Paper no.:

AIAA-2001-2252

Page(from):

1

Page(to):

10

Pages:

10

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050828
Series ID:	PA00000162
Conf. info. (Name):	AIAA/CEAS Aeroacoustics Conference
Conf. info. (Number):	7th
Conf. info. (Venue):	Maastricht, The Netherlands
Conf. info. (Date):	2001.05.28-2001.05.30
Note for article:	7th AIAA/CEAS Aeroacoustics Conference 28-30 May, 2001 Maastricht, The Netherlands

Similar Items:

1 Technical Paper Noise Computation of a Supersonic Shock-Containing Axisymmetric Jet by the CE/SE Method Loh, Ching Y., Hultgren, Lennart S., Chang, Sin-Chung, Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics	7 Technical Paper A 3-D CE/SE Navier-Stokes Solver with Unstructured Hexahedral Grid for Computation of Nearfield Jet Screech Noise Loh, C., Himansu, A., Hultgren, L. American Institute of Aeronautics and Astronautics
2 Technical Paper Computation of an Underexpanded 3-D Rectangular Jet by the CE/SE Method Loh,Ching Y., Himansu,Ananda, Wang,Xiao Y., Jorgenson,Philip C.E. American Institute of Aeronautics and Astronautics	8 Technical Paper Towards an 'all speed' unstructured upwind scheme Loh, Ching Y., Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics
3 Technical Paper Near-Field Noise Computation for a Supersonic Circular Jet Loh, C., Hultgren, L. American Institute of Aeronautics and Astronautics	9 Technical Paper Computing waves in compressible flow using the space-time conservation element and solution element method Loh, Ching Y., Hultgren, Lennart S., Chang, Sin-Chung American Institute of Aeronautics and Astronautics
4 Technical Paper Near-Field Noise Computation for a Subsonic Coannular Jet C. Loh, L. Hultgren, P. Jorgenson American Institute of Aeronautics and Astronautics	10 Technical Paper Robust and simple non-reflecting boundary conditions for the space-time conservation element and solution element method Chang, Sin-Chung, Loh, Ching Y., Yu, Sheng-Tao, Himansu, Ananda, Wang, Xiao-Yen, Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics
5 Technical Paper Vortex dynamics simulation in aeroacoustics by the space-time conservation element and solution element method Loh, Ching Y., Hultgren, Lennart S., Chang, Sin-Chung, Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics	11 Technical Paper High-resolution genuinely multidimensional solution of conservation laws by the space-time conservation element and solution element method Himansu, Ananda, Chang, Sin-Chung, Yu, Sheng-Tao, Wang, Xiao-Yen, Loh, Ching-Yuen, Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics
6 Technical Paper Vortex Dynamics Simulation in Aeroacoustics by the Space-Time Conservation Element and Solution Element Method Loh, Ching Y., Hultgren, Lennart S., Chang, Sin-Chung, Jorgenson, Philip C. E. American Institute of Aeronautics and Astronautics	12 Technical Paper High-Resolution Genuinely Multidimensional Solution of Conservation Laws by the Space-Time Conservation Element and Solution Element Method Himansu, Ananda, Chang, Sin-Chung, Yu, Sheng-Tao, Wang, Xiao-Yen, Loh, Ching-Yuen, Jorgenson, Philip C.E. American Institute of Aeronautics and Astronautics

1

2

3

4

5

6

7

8

9

10

11

12