University of Minnesota Ph.D. dissertation. 2021. Major: Aerospace Engineering and Mechanics. Advisor: Graham Candler. 1 computer file (PDF); 98 pages.Thermal protection systems made of ablative materials are a well-known solution to protect vehicles from high heating environments. As the material changes shape due to the ablation process, several patterns may develop. One pattern that develops is a very regularly ordered diamond-shaped pattern known as crosshatching. The mechanism for which initiates the pattern development is not yet known. This research aims to study the ablation process and its contribution to crosshatching by implementing and validating a camphor sublimating boundary condition into the US3D fluid-solid solver. This wor...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
The interaction of a turbulent boundary layer with an ablative surface is known to produce cross-hat...
Generalized method, including computer program, to solve problem of heat transfer and material respo...
A linear instability theory was developed which couples small perturbations in surface shape of a su...
The main objective of the present work is to demonstrate a method for prediction of aerothermal envi...
University of Minnesota Ph.D. dissertation. September 2017. Major: Mechanical Engineering. Advisor: ...
textA one-dimensional, quasi-steady ablation model with finite rate surface chemistry and frozen equ...
A unique numerical method has been developed for solving one-dimensional ablation heat transfer prob...
Problems involving mesh motion-which should not be mistakenly associated with moving mesh methods, a...
A linear instability theory was developed which couples small perturbations in surface shape of a su...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Space vehicles, while entering the planetary atmosphere, experience high loads of heat. Ablative mat...
The present thesis provides a description of historical and current modeling methods with recent dis...
University of Minnesota Ph.D. dissertation. May 2017. Major: Aerospace Engineering and Mechanics. Ad...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
The interaction of a turbulent boundary layer with an ablative surface is known to produce cross-hat...
Generalized method, including computer program, to solve problem of heat transfer and material respo...
A linear instability theory was developed which couples small perturbations in surface shape of a su...
The main objective of the present work is to demonstrate a method for prediction of aerothermal envi...
University of Minnesota Ph.D. dissertation. September 2017. Major: Mechanical Engineering. Advisor: ...
textA one-dimensional, quasi-steady ablation model with finite rate surface chemistry and frozen equ...
A unique numerical method has been developed for solving one-dimensional ablation heat transfer prob...
Problems involving mesh motion-which should not be mistakenly associated with moving mesh methods, a...
A linear instability theory was developed which couples small perturbations in surface shape of a su...
Re-entry of a spacecraft occurs at the hypersonic regime where the flow field is extremely complex: ...
Space vehicles, while entering the planetary atmosphere, experience high loads of heat. Ablative mat...
The present thesis provides a description of historical and current modeling methods with recent dis...
University of Minnesota Ph.D. dissertation. May 2017. Major: Aerospace Engineering and Mechanics. Ad...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Mechanical Engineering, 1995.Includes...
Re-entry of a spacecraft occurs at hypersonic regime where flow field is extremely complex. High tem...
The interaction of a turbulent boundary layer with an ablative surface is known to produce cross-hat...