Add to ORKGThis paper details the process of modeling and importing the model into FEA for the spun structure of the BS376 spacecraft. Engineering drawings were converted into 3D models using Pro/Engineer and then imported and into Patran for pre-processing of a Finite Element Model. To verify the Finite Element Model, several test cases were set up and solved using Nastran solver. Our simple load cases were found to be in congruence with analytical solution methods validating the finite element model
Two test cells were constructed to validate the ASHRAE cooling load calculation procedures developed...
The work presented here is a continuation of the Illini Air Shuttle project, focused on furthering ...
Various types of finite elements have been used in the prediction of critical speeds of turbomachine...
The X-33 vehicle is an advanced technology demonstrator sponsored by NASA. For the past 3 years the ...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This project proposes a new model for material removal rate (MRR) of conductive materials using die-...
This work focuses on using a reactive layered Al/Ni foil as a localized heat source for electronic ...
This thesis develops a finite element based dynamic modeling method for design and analysis of compl...
In this work the problem of performing a numerical simulation of quasi-static crack propagation with...
Particulate systems have been widely studied because of its various phenomena and tight relationship...
The electrodeposition of iron-group alloys has been widely studied due to their interest as material...
Foundation heat exchangers (FHX) are an alternative to more costly ground heat exchangers utilized i...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Materials Science and Engineering, 19...
Two test cells were constructed to validate the ASHRAE cooling load calculation procedures developed...
The work presented here is a continuation of the Illini Air Shuttle project, focused on furthering ...
Various types of finite elements have been used in the prediction of critical speeds of turbomachine...
The X-33 vehicle is an advanced technology demonstrator sponsored by NASA. For the past 3 years the ...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This paper describes the advantages, disadvantages, and complications that arise during the modeling...
This project proposes a new model for material removal rate (MRR) of conductive materials using die-...
This work focuses on using a reactive layered Al/Ni foil as a localized heat source for electronic ...
This thesis develops a finite element based dynamic modeling method for design and analysis of compl...
In this work the problem of performing a numerical simulation of quasi-static crack propagation with...
Particulate systems have been widely studied because of its various phenomena and tight relationship...
The electrodeposition of iron-group alloys has been widely studied due to their interest as material...
Foundation heat exchangers (FHX) are an alternative to more costly ground heat exchangers utilized i...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Materials Science and Engineering, 19...
Two test cells were constructed to validate the ASHRAE cooling load calculation procedures developed...
The work presented here is a continuation of the Illini Air Shuttle project, focused on furthering ...
Various types of finite elements have been used in the prediction of critical speeds of turbomachine...