Design of a Mach 3 Nozzle for TBCC Testing in the NASA LaRC 8-Ft High Temperature Tunnel

Design of a Mach 3 Nozzle for TBCC Testing in the NASA LaRC 8-Ft High Temperature Tunnel

Author(s):

R. Gaffney ( NASA Langley Research Center, Hampton, VA )
A. Norris

Publication title:

AIAA meeting papers on disc

Title of ser.:

AIAA Paper : AIAA Aerodynamic Measurement Technology and Ground Test Conference

Ser. no.:

2008

Pub. Year:

2008

No.:

2008-3703

Paper no.:

AIAA Paper 2008-3703

Pub. info.:

Reston, Va.: American Institute of Aeronautics and Astronautics

ISSN:

10877215

Language:

English

Call no.:

A07400/200807 [CD-ROM 2008 Disc 7]

Type:

Technical Paper

Details

TDL ID:	ZA00050893
Series ID:	PA00000165
Conf. info. (Name):	AIAA Aerodynamic Measurement Technology and Ground Testing Conference
Conf. info. (Number):	26th
Conf. info. (Venue):	Seattle, WA
Conf. info. (Date):	2008.06.23-2008.06.26
Note for article:	26th AIAA Aerodynamic Measurement Technology and Ground Testing Conference, 23-26 June 2008, Seattle, Washington

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