A subscale test program to assess the vortex shedding driven instabilities in segmented solid rocket motors

A subscale test program to assess the vortex shedding driven instabilities in segmented solid rocket motors

Author(s):

Publication title:

AIAA paper

Title of ser.:

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

Ser. no.:

1997

Pub. Year:

1997

No.:

97-3247

Paper no.:

97-3247

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:	ZA00050849
Series ID:	PA00000151
Conf. info. (Name):	AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Conf. info. (Number):	33rd
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	1997.07.06-1997.07.09
Note for article:	33rd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, July 6-9, 1997/Seattle, WA

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