Direct Prediction of Liquid Rocket Combustion Instabilities with Emphasis Placed on Velocity-and Pressure-Coupled Responses.

Direct Prediction of Liquid Rocket Combustion Instabilities with Emphasis Placed on Velocity-and Pressure-Coupled Responses.

Author(s):

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit

Ser. no.:

2002

Pub. Year:

2002

No.:

2002-3698

Paper no.:

2002-3698

Pages:

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00001704
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	38th
Conf. info. (Venue):	Indianapolis, IN
Conf. info. (Date):	2002.07.07-2002.07.10
Note for article:	38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit, Indianapolis, Indiana, 7-10 July 2002

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