Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine

Flowrate and acoustics characteristics of coaxial swirling injector of hydrogen/oxygen rocket engine

Author(s):

Zhou, Jin ( National University of Defense Technology, P.R. China )
Hu, Xiaoping
Huang, Yuhui
Wang, Zhenguo

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

1996

Pub. Year:

1996

No.:

96-3135

Paper no.:

96-3135

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050840
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	32nd
Conf. info. (Venue):	Lake Buena Vista, FL
Conf. info. (Date):	1996.07.01-1996.07.03
Note for article:	32nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 1-3, 1996/Lake Buena Vista, FL

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