1–3 von 3 Ergebnissen
|

    Design and Viscous Correction of an Axisymmetric Contoured Nozzle for Perfect Gas to the T2 Hypersonic Shock Tunnel

    Vilela, Renan G. / Fraile Junior, Andre C. / Ribeiro, Lucas A. et al. | AIAA | 2023

      Design and Viscous Correction of an Axisymmetric Contoured Nozzle for Perfect Gas to the T2 Hypersonic Shock Tunnel

      Vilela, Renan G. / Junior, Andre C. Fraile / Ribeiro, Lucas A. et al. | TIBKAT | 2023

    A New Combustion-Driver 1.1 m Diameter Hypersonic Shock Tunnel to Simulate Mach 10 Flight Conditions

    Minucci, Marco A. / Rego, Israel / Vilela, Renan G. et al. | AIAA | 2023

      A New Combustion-Driver 1.1 M Diameter Hypersonic Shock Tunnel to Simulate Mach 10 Flight Conditions

      Minucci, Marco A. / Rego, Israel / Vilela, Renan G. et al. | TIBKAT | 2023

    Experimental Flowpath Characterization of the T2 Shock Tunnel Mach 7.0 Hybrid Axisymmetric Contour Nozzle

    Vilela, Renan G. / Ribeiro, Lucas A. / Rego, Israel et al. | AIAA | 2024