An Improved Turbulent Boundary-Layer Model for Shock Tubes

An Improved Turbulent Boundary-Layer Model for Shock Tubes

Author(s):

Petersen,E.L. ( Propulsion Science & Experimental Mechanics The Aerospace Corporation )
Hanson,R.K. ( Department of Mechanical Engineering Stanford University )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : AIAA Fluid Dynamics Conference

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-2855

Paper no.:

AIAA-2001-2855

Page(from):

1

Page(to):

13

Pages:

13

Pub. info.:

Reston, VA: American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050823
Series ID:	PA00000147
Conf. info. (Name):	AIAA Fluid Dynamics Conference & Exhibit
Conf. info. (Number):	31st
Conf. info. (Venue):	Anaheim, CA
Conf. info. (Date):	2001.06.11-2001.06.14
Note for article:	31st AIAA Fluid Dynamics Conference & Exhibit 11-14 June 2001/Anaheim, CA

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