Great thanks goes to my advisor Graham Candler, who gave me a chance to prove myself in graduate school, to Ioannis Nompelis who fueled my interest in the simulation sciences, and all of the colleagues from whom I harvested much useful knowledge and expertise. i Dedication To my sweet wife Bonnie. ii A method is developed for performing simulations that contain fluid-structure interac-tions between deployable decelerators and a high speed compressible flow. The prob-lem of coupling together multiple physical systems is examined with discussion of the strength of coupling for various methods. A non-monolithic strongly coupled option is presented for fluid-structure systems based on grid deformation. A class of algebraic grid deformation meth...
<p align="justify">This work deals with the development of numerical methods for compressible flow s...
The work presented concerns the numerical simulation on the dynamic behaviour of full size parachute...
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and ...
A validated computational fluid-structure interaction method for simulating the complex interaction ...
A series of fluid-structure interaction simulations of an aerodynamic tension-cone supersonic decele...
This paper describes large-scale simulations of compressible flows over a supersonic disk-gap-band p...
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and ...
The landing of the Mars Science Laboratory (MSL) in 2012 demonstrated the limits of supersonic plane...
Fluid-Structure Interaction (FSI) problems are of great importance to many fields of engineering and...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
Inflatable aerodynamic decelerators present potential advantages for planetary entry in missions of ...
The interaction between a flexible structure and the surrounding fluid gives rise to a variety of ph...
In this doctoral work, we adress various problems arising when dealing with multi-physical simulatio...
The design of future light aerospace structures will require numerical tools to ac-curately describe...
Accurate measurementsof the aerodynamic performance in wind tunnel experiments require to retain dyn...
<p align="justify">This work deals with the development of numerical methods for compressible flow s...
The work presented concerns the numerical simulation on the dynamic behaviour of full size parachute...
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and ...
A validated computational fluid-structure interaction method for simulating the complex interaction ...
A series of fluid-structure interaction simulations of an aerodynamic tension-cone supersonic decele...
This paper describes large-scale simulations of compressible flows over a supersonic disk-gap-band p...
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and ...
The landing of the Mars Science Laboratory (MSL) in 2012 demonstrated the limits of supersonic plane...
Fluid-Structure Interaction (FSI) problems are of great importance to many fields of engineering and...
Thesis (S.M.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 2004.In...
Inflatable aerodynamic decelerators present potential advantages for planetary entry in missions of ...
The interaction between a flexible structure and the surrounding fluid gives rise to a variety of ph...
In this doctoral work, we adress various problems arising when dealing with multi-physical simulatio...
The design of future light aerospace structures will require numerical tools to ac-curately describe...
Accurate measurementsof the aerodynamic performance in wind tunnel experiments require to retain dyn...
<p align="justify">This work deals with the development of numerical methods for compressible flow s...
The work presented concerns the numerical simulation on the dynamic behaviour of full size parachute...
Inflatable aerodynamic decelerators have potential advantages for planetary re-entry in robotic and ...