Gaseous piston effect in shock tube/tunnel when operating in the equilibrium interface condition.
A new and promising technique for improving shock tube/tunnel performance is presented. This technique is able to produce higher reservoir enthalpy levels than the ones usually obtained with conventional shock tubes/tunnels, when operating in the Equilibrium Interface Condition. The new technique, w...
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| Format: | Others |
| Language: | English |
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Instituto Tecnológico de Aeronáutica
1997
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| Online Access: | http://www.bd.bibl.ita.br/tde_busca/arquivo.php?codArquivo=1392 |