Computational analysis of hypersonic inlet flow in a rocket-based combined-cycle engine

Computational analysis of hypersonic inlet flow in a rocket-based combined-cycle engine

Author(s):

Yungster, S. ( ICOMP, NASA Lewis Research Center )
DeBonis, J.R.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1997

Pub. Year:

1997

No.:

97-0028

Paper no.:

97-0028

Page(from):

1

Page(to):

13

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050850
Series ID:	PA00000138
Conf. info. (Name):	Aerospace Sciences Meeting and Exhibit
Conf. info. (Number):	35th
Conf. info. (Venue):	Reno, NV
Conf. info. (Date):	1997.01.06-1997.01.10
Note for article:	35th Aerospace Sciences Meeting & Exhibit, January 6-10, 1997/Reno, NV

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