Experimental Investigations of Test Gas Effects on the Hypersonic Flow Field Around Large Angle Blunt Cone in Shock Tunnel

Experimental Investigations of Test Gas Effects on the Hypersonic Flow Field Around Large Angle Blunt Cone in Shock Tunnel

Author(s):

Jagadeesh,G. ( Shock Wave Research Center, IFS, Tohoku University )
Sun,M. ( Dept. of Aerosapce Engineering, Indian Institute Of Science )
Nagashetty,K.
Reddy,K.P.J.

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

2001

Pub. Year:

2001

No.:

2001-0305

Paper no.:

AIAA-2001-0305

Page(from):

1

Page(to):

9

Pages:

9

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper

Details

TDL ID:	ZA00050880
Series ID:	PA00000138
Conf. info. (Name):	AIAA Aerospace Sciences Meeting & Exhibit
Conf. info. (Number):	39th
Conf. info. (Venue):	Reno, Nevada
Conf. info. (Date):	2001.01.08-2001.01.11
Note for article:	39th AIAA Aerospace Sciences Meeting & Exhibit 8-11 January 2001/Reno, NV

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