Ask
Search
My library
ORKG

ORKG Ask

Our mission is to organize scholarly knowledge and make it accessible to humans and machines.

About

About ORKG Ask
Report issue
Statistics
Contact

Legal

Terms of use
Data protection (sheet)
Imprint
Accessibility
License

Technical

We
open source
System status
Changelog
Frontend: v1.41.0
Backend: v1.13.4

We use cookies to provide a better user experience.

Data Protection

Strongly coupled computation of material response and nonequilibrium flow for hypersonic ablation

Martin, Alexandre
Boyd, Iain D.

Publication date

January 2009

DOI

10.2514/6.2009-3597

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Language

English

Citation count (estimate)

1

Abstract

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77076/1/AIAA-2009-3597-202.pd

Extracted data

Related items

Implementation of Radiation, Ablation, and Free Energy minimization Modules for Coupled Simulations of Hypersonic Flow,” AIAA Paper 2009-1399

Peter A Gnoffo
Christopher O Johnston
Richard A. Thompson

January 2009

A description of models and boundary conditions required for coupling radiation and ablation physics...

Implicit Coupling Approach for Simulation of Charring Carbon Ablators

Gokcen, Tahir
Chen, Yih-Kanq

June 2013

This study demonstrates that coupling of a material thermal response code and a flow solver with non...

Development of an Unstructured Navier-Stokes Solver for Hypersonic Nonequilibrium Aerothermodynamics

Scalabrin, Leonardo
Boyd, Iain D.

January 2005

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76685/1/AIAA-2005-5203-455.pd

Implicit Implementation of Material Response and Moving Meshes for Hypersonic Re-entry Ablation

Martin, Alexandre
Boyd, Iain D.

January 2009

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd

Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation

Martin, Alexandre
Boyd, Iain D.

October 2014

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd

Re Martin
Iain D. Boyd
A Jacobian Matrix
F Inviscid Flux Vector
Fd Diffusive Flux Vector
Fo Forchheimer Number
S S Surface
Tv Vibrational Temperature
U Conservative Vector

January 2016

A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...

Coupled Computation of Fluid and Material Response for Non-Charring Ablative Materials in Hypersonic Flow

Wiebenga, Jonathan E.
Boyd, Iain D.

February 2012

Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...

Computation of Multi-Dimensional Material Response Coupled to Hypersonic Flow

Wiebenga, Jonathan
Boyd, Iain

January 2012

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97085/1/AIAA2012-2873.pd

Simulation of Ablating Hypersonic Vehicles with Finite-Rate Surface Chemistry

Farbar, Erin D.
Alkandry, Hicham
Wiebenga, Jonathan
Boyd, Iain D.

June 2014

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd

Simulation of Pyrolysis Gas Within a Thermal Protection System

Martin, Alexandre
Boyd, Iain D.

January 2008

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd

Numerical Investigation of Three-Dimensional Effects within a Charring Ablator

Martin, Alexandre
Khan, Ovais U.
Zhang, Huai-Bao

February 2012

Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...

Computational Modelling of High-Temperature Gas Effects with Application to Hypersonic Flows

Rowan Gollan

June 2008

During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...

Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations

Scalabrin, Leonardo
Boyd, Iain D.

January 2006

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76521/1/AIAA-2006-3773-970.pd

Coupled Flow Field Simulations of Charring Ablators with Nonequilibrium Surface Chemistry

Alkandry, Hicham
Boyd, Iain D.
Martin, Alexandre

June 2013

This paper describes the coupling of a Navier-Stokes solver to a material response code to simulate ...

Modeling and Numerical Simulation of the Behavior of Charring Ablators During Atmospheric Re-Entry

DAL BIANCO, ALESSANDRA

January 2013

During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...

Implementation of Radiation, Ablation, and Free Energy minimization Modules for Coupled Simulations of Hypersonic Flow,” AIAA Paper 2009-1399

Peter A Gnoffo
Christopher O Johnston
Richard A. Thompson

January 2009

A description of models and boundary conditions required for coupling radiation and ablation physics...

Implicit Coupling Approach for Simulation of Charring Carbon Ablators

Gokcen, Tahir
Chen, Yih-Kanq

June 2013

This study demonstrates that coupling of a material thermal response code and a flow solver with non...

Development of an Unstructured Navier-Stokes Solver for Hypersonic Nonequilibrium Aerothermodynamics

Scalabrin, Leonardo
Boyd, Iain D.

January 2005

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76685/1/AIAA-2005-5203-455.pd

Implicit Implementation of Material Response and Moving Meshes for Hypersonic Re-entry Ablation

Martin, Alexandre
Boyd, Iain D.

January 2009

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/77158/1/AIAA-2009-670-901.pd

Strongly Coupled Computation of Material Response and Nonequilibrium Flow for Hypersonic Ablation

Martin, Alexandre
Boyd, Iain D.

October 2014

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140702/1/1.A32847.pd

Re Martin
Iain D. Boyd
A Jacobian Matrix
F Inviscid Flux Vector
Fd Diffusive Flux Vector
Fo Forchheimer Number
S S Surface
Tv Vibrational Temperature
U Conservative Vector

January 2016

A one-dimensional material response implicit solver with surface ablation and pyrolysis is strongly ...

Coupled Computation of Fluid and Material Response for Non-Charring Ablative Materials in Hypersonic Flow

Wiebenga, Jonathan E.
Boyd, Iain D.

February 2012

Hypersonic vehicles are subjected to high heat loads throughout their flight trajectories, and as a ...

Computation of Multi-Dimensional Material Response Coupled to Hypersonic Flow

Wiebenga, Jonathan
Boyd, Iain

January 2012

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/97085/1/AIAA2012-2873.pd

Simulation of Ablating Hypersonic Vehicles with Finite-Rate Surface Chemistry

Farbar, Erin D.
Alkandry, Hicham
Wiebenga, Jonathan
Boyd, Iain D.

June 2014

Peer Reviewedhttps://deepblue.lib.umich.edu/bitstream/2027.42/140434/1/6.2014-2124.pd

Simulation of Pyrolysis Gas Within a Thermal Protection System

Martin, Alexandre
Boyd, Iain D.

January 2008

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76855/1/AIAA-2008-3805-224.pd

Numerical Investigation of Three-Dimensional Effects within a Charring Ablator

Martin, Alexandre
Khan, Ovais U.
Zhang, Huai-Bao

February 2012

Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...

Computational Modelling of High-Temperature Gas Effects with Application to Hypersonic Flows

Rowan Gollan

June 2008

During atmospheric entry, a spacecraft's aeroshell uses a thermal protection system (TPS) to withsta...

Numerical Simulation of Weakly Ionized Hypersonic Flow for Reentry Configurations

Scalabrin, Leonardo
Boyd, Iain D.

January 2006

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76521/1/AIAA-2006-3773-970.pd

Coupled Flow Field Simulations of Charring Ablators with Nonequilibrium Surface Chemistry

Alkandry, Hicham
Boyd, Iain D.
Martin, Alexandre

June 2013

This paper describes the coupling of a Navier-Stokes solver to a material response code to simulate ...

Modeling and Numerical Simulation of the Behavior of Charring Ablators During Atmospheric Re-Entry

DAL BIANCO, ALESSANDRA

January 2013

During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...

Implementation of Radiation, Ablation, and Free Energy minimization Modules for Coupled Simulations of Hypersonic Flow,” AIAA Paper 2009-1399

Peter A Gnoffo
Christopher O Johnston
Richard A. Thompson

January 2009

A description of models and boundary conditions required for coupling radiation and ablation physics...

Implicit Coupling Approach for Simulation of Charring Carbon Ablators

Gokcen, Tahir
Chen, Yih-Kanq

June 2013

This study demonstrates that coupling of a material thermal response code and a flow solver with non...

Development of an Unstructured Navier-Stokes Solver for Hypersonic Nonequilibrium Aerothermodynamics

Scalabrin, Leonardo
Boyd, Iain D.

January 2005

Peer Reviewedhttp://deepblue.lib.umich.edu/bitstream/2027.42/76685/1/AIAA-2005-5203-455.pd