Noise Computation of a Supersonic Shock-Containing Axisymmetric Jet by the CE/SE Method

Noise Computation of a Supersonic Shock-Containing Axisymmetric Jet by the CE/SE Method

Author(s):

Loh, Ching Y. ( Taitech Inc. & NASA Glenn )
Hultgren, Lennart S.
Chang, Sin-Chung
Jorgenson, Philip C.E.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2000

Pub. Year:

2000

No.:

2000-0475

Paper no.:

00-0475

Page(from):

1

Page(to):

15

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050874
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospaces Science Meeting and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	2000.01.10-2000.01.13
Note for article:	38th Aerospace Sciences Meeting & Exhibit 10-13 January 2000 / Reno, NV

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