101–108 von 108 Ergebnissen
|

    Flow Interaction Dynamics of Stagnation Point Injection in Mach 6 Quiet Flow

    Mejia, Nicholas / Schmidt, Bryan E. / DeFazio, Dominick et al. | AIAA | 2024

    Computational Prediction of Pressure and Thermal Environments in the Flame Trench with Launch Vehicles

    Brehm, Christoph / Sozer, Emre / Moini-Yekta, Shayan et al. | AIAA | 2013

      Computational Prediction of Pressure and Thermal Environments in the Flame Trench With Launch Vehicles

      Brehm, Christoph / Sozer, Emre / Barad, Michael F. et al. | NTRS | 2014

    High-fidelity CFD verification workshop 2024: wall-modeled large eddy simulation of smooth-body separation

    Larsson, Johan / Bermejo Moreno, Ivan / Baurle, Robert A. et al. | AIAA | 2023

      High-Fidelity CFD Verification Workshop 2024: Wall-modeled Large Eddy Simulation of Smoothbody Separation

      Larsson, Johan / Moreno, Ivan Bermejo / Baurle, Robert A. et al. | TIBKAT | 2023

    Assessment of Linear Methods for Analysis of Boundary Layer Instabilities on a Finned Cone at Mach 6

    Araya, Daniel / Bitter, Neal / Wheaton, Bradley M. et al. | AIAA | 2022

      Assessment of Linear Methods for Analysis of Boundary Layer Instabilities on a Finned Cone at Mach 6

      Araya, Daniel / Bitter, Neal / Wheaton, Bradley M. et al. | TIBKAT | 2022

    High Enthalpy Effects on Hypersonic Boundary-Layer Transition: T5 Experimental and Numerical Comparison

    Hameed, Ahsan / Chen, James H. / Parziale, Nick J. et al. | AIAA | 2024

    Ground Tests on the BOLT Geometry at Mach 6 and 7: Cross-Facility Comparison and Stability Analysis

    Butler, Cameron / Wheaton, Bradley M. / Li, Fei et al. | AIAA | 2024

    1/5 Scale Model of Aeromot 200S SuperXimango for Scaled Flight Research

    Gross, Andreas / Pearman, Cory / Kremer, Rodney et al. | AIAA | 2008

    High Enthalpy Effects on Hypersonic Boundary Layer Transition

    Wartemann, Viola / Wagner, Alexander / Tanno, Hideyuki et al. | AIAA | 2024