Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle

Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle

Author(s):

Publication title:

A collection of technical papers : 10th International Space Planes and Hypersonic Systems and Technologies Conference, Kyoto, Japan, 24-27 April 2001

Title of ser.:

AIAA Paper : International Space Planes and Hypersonic Systems and Technologies Conference

Ser. no.:

2001

Pub. Year:

2001

Vol.:

v. 1

No.:

2001-1811

Paper no.:

AIAA-2001-1811

Page(from):

308

Page(to):

317

Pages:

10

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISBN:

9781563474781 [1563474786]

Language:

English

Call no.:

A07400/011750

Type:

Technical Paper

Details

TDL ID:	ZA00000082
Series ID:	PA00000152
Conf. info. (Name):	International Space Planes and Hypersonic Systems and Technologies Conference
Conf. info. (Number):	10th
Conf. info. (Venue):	Kyoto, Japan
Conf. info. (Date):	2001.04.24-2001.04.27

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