Hypersonic test facilities available in Western Europe for aerodynamic/aerothermal and structure/material investigations-Reference-Cited by-同舟云学术

Hypersonic test facilities available in Western Europe for aerodynamic/aerothermal and structure/material investigations

Published:1999-08 Issue:1759 Volume:357 Page:2227-2248
ISSN:1364-503X
Container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences
language:en
Short-container-title:Philosophical Transactions of the Royal Society of London. Series A: Mathematical, Physical and Engineering Sciences

Author:

Vennemann Dietrich¹

Affiliation:

1. European Space Agency, ESTEC, Keplerlaan 1, 2200 AG Noordwijk, The Netherlands

Publisher

The Royal Society

Subject

General Physics and Astronomy,General Engineering,General Mathematics

Link

https://royalsocietypublishing.org/doi/pdf/10.1098/rsta.1999.0429

Reference19 articles.

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2. Bottin B. & Carbonaro M. 1997 Potential applications of induction heating to aerospace technologies in the 1.2 MW plasmatron of the von Karman Institute. In Congres Int. sur l'induction dans les procedes industriels Paris France 27-29 Mai.

3. Bottin B. Carbonaro M. Zemsch S. & Degrez G. 1997a Design of a new inductively-coupled plasma wind tunnel for re-entry material testing at the von Karman Institute. In Wind tunnels and wind tunnel test techniques Cambridge UK 14-16 April.

4. Aerothermodynamic design of an inductively coupled plasma wind tunnel;Bottin B.;AIAA,1997

5. Caristia S. Tamai R. Risch T. & Isaacson P. 1995 SCIROCCO project-plasma wind tunnel to support spacecraft testing under construction in Italy. ITEA J. December 1995/January 1996 5.

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