Numerical analysis of rocket turbopump inducer at cryogenic homogeneous two-phase flow conditions

Numerical analysis of rocket turbopump inducer at cryogenic homogeneous two-phase flow conditions

Author(s):

Akmandor, I. Sinan ( Middle East Technical University )
Nagashima, Toshio ( University of Tokyo )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1999

Pub. Year:

1999

No.:

99-0874

Paper no.:

99-0874

Page(from):

1

Page(to):

10

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050873
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	37th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1999.01.11-1999.01.14
Note for article:	37th AIAA Aerospace Sciences Meeting and Exhibit, January 11-14, 1999/Reno, NV

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