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Inlet development for a rocket based combined cycle, single stage to orbit vehicle using computational fluid dynamics

Author(s):
Publication title:
AIAA paper
Title of ser.:
AIAA Paper : AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit
Ser. no.:
1999
Pub. Year:
1999
No.:
99-2239
Paper no.:
99-2239
Page(from):
1
Page(to):
18
Pub. info.:
American Institute of Aeronautics and Astronautics
ISSN:
01463705
Language:
English
Call no.:
A07400
Type:
Technical Paper

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