The 4th edition (2011) of the Ablation Modeling workshop focuses on the experimental support required for the development and validation of high fidelity models in the following areas: In-depth physics and chemistry of ablation Gas-surface interactions and catalysis Roughness modeling including wall-blowing effects Ablation models inter-code calibration and validation Poster session dedicated to various existing modeling efforts The emphasis for each of the target areas is the material contribution as opposed to the aerothermodynamics. With the workshop being the first non-ITAR edition we are seeking to expose the broader (national and international) community to the particular issues involved with material response modeling under hypers...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
National interest in hypersonic flight provides the motivation to develop closure models for high-sp...
textA one-dimensional, quasi-steady ablation model with finite rate surface chemistry and frozen equ...
Ablative thermal protection materials are a key technology for current and future space exploration ...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
The collection of methods described in this manuscript can be used in a dynamic simulation to provid...
Several high-fidelity material-response models are being developed by the hypersonic community. Thes...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Ground testing of ablative materials aims at providing critical data on the material behavior under ...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
This talk will overview ablation modeling and simulation at Sandia National Laboratories, past, pres...
The test-case series #3 will be a further extension of the tests defined within the framework of the...
Designing thermal protection systems (TPS) for ballistic re-entry capsules requires both reliable nu...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
National interest in hypersonic flight provides the motivation to develop closure models for high-sp...
textA one-dimensional, quasi-steady ablation model with finite rate surface chemistry and frozen equ...
Ablative thermal protection materials are a key technology for current and future space exploration ...
In the late 1950s, the earliest models describing the thermal response of ablative materials were ba...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
The collection of methods described in this manuscript can be used in a dynamic simulation to provid...
Several high-fidelity material-response models are being developed by the hypersonic community. Thes...
During the atmospheric entry of a blunt body, a bow shock wave is generated on the nose of the vehic...
Ground testing of ablative materials aims at providing critical data on the material behavior under ...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
This talk will overview ablation modeling and simulation at Sandia National Laboratories, past, pres...
The test-case series #3 will be a further extension of the tests defined within the framework of the...
Designing thermal protection systems (TPS) for ballistic re-entry capsules requires both reliable nu...
We are interested in participating in the inter-code calibration and validation exercise in the Four...
Low-density carbon/phenolic is a class of ablative materials that is attractive for blunt body space...
National interest in hypersonic flight provides the motivation to develop closure models for high-sp...
textA one-dimensional, quasi-steady ablation model with finite rate surface chemistry and frozen equ...