Compressibility Considerations for k-w Turbulence Models in Hypersonic Boundary-Layer Applications

2010/01/01 by Christopher L. Rumsey · 82 citations
Engineering · Mathematics · #Aerospace engineering #Boundary layer #Compressibility #Computational Fluid Dynamics and Aerodynamics #Computer science #Engineering #Fluid Dynamics and Turbulent Flows #Gas Dynamics and Kinetic Theory #Hypersonic speed #Mechanical engineering #Mechanics #Missile #Physics #Space (punctuation) #Space Shuttle #Spacecraft #Spacecraft design #Systems engineering #Turbulence

paper · doi:10.2514/1.45350

published in Journal of Spacecraft and Rockets 47(1), 11-20 (American Institute of Aeronautics and Astronautics)

openalex publication_date 2010/01/01 · openalex created_date 2025/10/10 · openalex updated_date 2026/07/23

Abstract

Covers advancements in spacecraft and tactical and strategic missile systems, including subsystem design and application, mission design and analysis, materials and structures, developments in space sciences, space processing and manufacturing, space operations, and applications of space technologies to other fields.

Citations

• Two-equation eddy-viscosity turbulence models for engineering applications

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