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physics.flu-dyn2025

Verification of Convergent-Divergent Nozzle Designs in Propulsion Aerospace Applications

Noah L. Estrada, Marc A. Cantu, Arturo Rodriguez +5

The performance of convergent and divergent nozzles is critical in aerospace propulsion systems, where the efficient expansion of high-temperature, high-pressure gases directly imp…

physics.flu-dyn2025

Computational Aerothermal Framework and Analysis of Stetson Mach 6 Blunt Cone

Arturo Rodriguez, Piyush Kumar, Cesar Diaz-Caraveo +4

Accurately predicting aerothermal behavior is paramount for the effective design of hypersonic vehicles, as aerodynamic heating plays a pivotal role in influencing performance metr…

physics.flu-dyn2024

Current State of Atmospheric Turbulence Cascades

Vicente Corral Arreola, Arturo Rodriguez, Vinod Kumar

Turbulence cascade has been modeled using various methods; the one we have used applies to a more exact representation of turbulence where people use the multifractal representatio…

physics.flu-dyn2024

Designing an Optimal Scoop for Holloman High-Speed Test Track Water Braking Mechanism using Computational Fluid Dynamics

Jose A. Terrazas, Piyush Kumar, Arturo Rodriguez +3

Specializing in high-speed testing, Holloman High-Speed Test Track (HHSTT) uses water braking to stop vehicles on the test track. This method takes advantage of the higher density…

physics.flu-dyn2024

Computational Investigation of Roughness Effects on Boundary Layer Transition for Stetson's Blunt Cone at Mach 6

Arturo Rodriguez, Piyush Kumar, Cesar Diaz-Caraveo +3

In this aerothermal study, we performed a two-dimensional steady-state Computational Fluid Dynamics (CFD) and heat conduction simulation at Mach 6. The key to our methodology was a…