Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations

By Leonardo C. Scalabrin, Iain D. Boyd. 2006

237 citations recorded by the source corpus.

Subfields: Aerospace Engineering, Applied Mathematics, Computational Mechanics

View Paper: https://www.semanticscholar.org/paper/c1425c2ee0fb186340eda49596c912feabb5a7f6

How researchers see this paper

The researchers whose trusted networks rank it highest, strongest advocate first. Every researcher gets a different order.

In Aerospace Engineering

1. A. Lofthouse
2. Iain D. Boyd
3. Leonardo C. Scalabrin

In Applied Mathematics

1. A. Lofthouse
2. Iain D. Boyd
3. Leonardo C. Scalabrin

In Computational Mechanics

1. A. Lofthouse
2. Iain D. Boyd
3. Leonardo C. Scalabrin

Citations in the corpus

• Electromagnetic Reduction of Plasma Density During Atmospheric Reentry and Hypersonic Flights (2008, background): “More details about hypersonic flow simulations can be found in [17,18].”
• Velocity Slip and Temperature Jump in Hypersonic Aerothermodynamics (2007, methodology): “The CFD results are obtained using the Michigan aerothermodynamic Navier–Stokes (LeMANS) code, developed for the simulation of hypersonic reactingflowfields [11,12].”