Direct numerical simulation on the receptivity, instability, and transition of hypersonic boundary layers
The prediction of the laminar-turbulent transition of boundary layers is critically important to
the development of hypersonic vehicles because the transition has a first-order impact on …
the development of hypersonic vehicles because the transition has a first-order impact on …
Hypersonics into the 21st century: A perspective on AFOSR-sponsored research in aerothermodynamics
JD Schmisseur - Progress in Aerospace Sciences, 2015 - Elsevier
This paper documents the programmatic context and considerations that have shaped the
development and execution of a number of research initiatives implemented by the Air Force …
development and execution of a number of research initiatives implemented by the Air Force …
[PDF][PDF] Numerical simulation of weakly ionized hypersonic flow over reentry capsules
LC Scalabrin - 2007 - Citeseer
The aging of the Space Shuttle prompted significant research on possible designs for its
replacement through the years. For a long time it was believed that the replacement for this …
replacement through the years. For a long time it was believed that the replacement for this …
SU2-NEMO: An open-source framework for high-Mach nonequilibrium multi-species flows
SU2-NEMO, a recent extension of the open-source SU2 multiphysics suite's set of physical
models and code architecture, is presented with the aim of introducing its enhanced …
models and code architecture, is presented with the aim of introducing its enhanced …
Computational Fluid Dynamics of a Radial Compressor Operating With Supercritical CO2
The merit of using supercritical CO 2 (scCO 2) as the working fluid of a closed Brayton cycle
gas turbine is now widely recognized, and the development of this technology is now …
gas turbine is now widely recognized, and the development of this technology is now …
Reynolds-averaged Navier-Stokes simulations of the HyShot II scramjet
THE development of computational tools that can faithfully reproduce high-Mach-number
flight conditions is fundamental to improving our ability to realize hypersonic vehicles …
flight conditions is fundamental to improving our ability to realize hypersonic vehicles …
Finite-rate and equilibrium study of graphite ablation under arc-jet conditions
Arc-jet facilities play a primary role in recreating aerothermal conditions experienced by
atmospheric entry vehicles and are widely used to test the performance of thermal protection …
atmospheric entry vehicles and are widely used to test the performance of thermal protection …
High performance modeling of atmospheric re-entry vehicles
Re-entry vehicles designed for space exploration are usually equipped with thermal
protection systems made of ablative material. In order to properly model and predict the …
protection systems made of ablative material. In order to properly model and predict the …
A two-temperature open-source CFD model for hypersonic reacting flows, part one: zero-dimensional analysis
A two-temperature CFD (computational fluid dynamics) solver is a prerequisite to any
spacecraft re-entry numerical study that aims at producing results with a satisfactory level of …
spacecraft re-entry numerical study that aims at producing results with a satisfactory level of …
Strongly coupled computation of material response and nonequilibrium flow for hypersonic ablation
The steps necessary to achieve the strong coupling between a flowfield solver and a
material response solver are presented. This type of coupling is required to accurately …
material response solver are presented. This type of coupling is required to accurately …