Hypersonic gaseous piston shock tunnel: numerical and experimental results

Author(s):

• do Nascimento, M.A.C. ( Laboratory of Aerothermodynamics and Hypersonics, IEAv-CTA )
• Minucci, M.A.S. ( Laboratory of Aerothermodynamics and Hypersonics, IEAv-CTA )
• Ramos, A.G. ( Laboratory of Aerothermodynamics and Hypersonics, IEAv-CTA )
• Chanes, J.B., Jr. ( Laboratory of Aerothermodynamics and Hypersonics, IEAv-CTA )
• Nagamatsu, H.T. ( Department of Mechanical Engineering, Aeronautical Engineering and Mechanics, Rensselaer Polytechnic Institute )

Publication title:

AIAA paper

Title of ser.:

AIAA Paper : Aerospace Sciences Meeting and Exhibit

Ser. no.:

1998

Pub. Year:

1998

No.:

98-0548

Paper no.:

98-0548

Page(from):

1

Page(to):

7

Pub. info.:

American Institute of Aeronautics and Astronautics

ISSN:

01463705

Language:

English

Call no.:

A07400

Type:

Technical Paper