The Thermal Response of an Internal Flow in a Solid Rocket Motor Chamber/Nozzle Model

The Thermal Response of an Internal Flow in a Solid Rocket Motor Chamber/Nozzle Model

Author(s):

Hegab,A.M. ( Department of Aeronautical and Astronautical Engineering University of Illinois )
Kassoy,D.R. ( Center for Combustion Research University of Colorado )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-0338

Paper no.:

AIAA-2001-0338

Page(from):

1

Page(to):

15

Pages:

15

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050880
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting & Exhibit
Conf. info. (Number):	39th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2001.01.08-2001.01.11
Note for article:	39th AIAA Aerospace Sciences Meeting & Exhibit 8-11 January 2001/Reno, NV

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