PG-EAM - Graduate Program in Aeronautical and Mechanical Engineering
PT EN
PhD Thesis 1997

Gaseous piston effect in shock tube/tunnel when operating in the equilibrium interface condition.

Author

Marco Antonio Couto do Nascimento

Advisors

  • Advisor Marco Antonio Sala Minucci
  • Co-advisor Paulo Afonso de Oliveira Soviero

Concentration Area

Aerodinâmica, Propulsão e Energia

Defense Date

1997

Thesis Number

000386270

Abstract

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, which is tentatively being called "Gaseous Piston Technique", has been proven also to prevent combustion from taking place at the air-hydrogen interface, and seems to be capable to improve the available testing time by reducing the test gas contamination by the driver gas. The qualitative agreement of both numerical and experimental investigations is very encouraging.

Keywords

Túneis de choque Tubos de choque Dinâmica dos gases Escoamento hipersônico Aerodinâmica Engenharia aeronáutica Física