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Caitlyn McKay. Structures and Thermal Locomotion Phase. 1. Using a Crushable Material. 2. Updated Rover. Total Mass = 17.4 kg. 3. Global Buckling Cylinder. 4. 5. Impulse Momentum. 6. 7. Load on Curve Beam (wheel spoke). 8. 9. Buckling of Aluminum Body.
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Caitlyn McKay Structures and Thermal Locomotion Phase 1
Using a Crushable Material Caitlyn McKay Structures and Thermal 2
Updated Rover Total Mass = 17.4 kg 3 Caitlyn McKay Structures and Thermal
Global Buckling Cylinder 4 Caitlyn McKay Structures and Thermal
5 Caitlyn McKay Structures and Thermal
Impulse Momentum 6 Caitlyn McKay Structures and Thermal
7 Caitlyn McKay Structures and Thermal
Load on Curve Beam (wheel spoke) Caitlyn McKay Structures and Thermal 8
9 Caitlyn McKay Structures and Thermal
Buckling of Aluminum Body Buckling Stress: 712 kg/m^2 10 Caitlyn McKay Structures and Thermal
Shear Stress on Motor Shaft 11 Caitlyn McKay Structures and Thermal
References: 12 Caitlyn McKay Structures and Thermal 2008. CES EduPack2008. Citrix Client. Purdue University, West Lafayette, IN. Grandt, Alten F. Fundamentals of Structural Integrity. 28-45. Hoboken, NJ: John Wiley & Sons, Inc., 2004. Gere, James M. Mechanics of Materials. 6th ed. Belmont: Brooks/Cole, 2003.
13 Caitlyn McKay Structures and Thermal Gonza´lez, Carlos, and Javier LLorca. "Stiffness of a curved beam subjected to axial load." International Journal of Solids and Structures: 1537-1545. Elsevier. 13 Oct. 2004. Science Direct. 14 Feb. 2009 <www.elsevier.com/locate/ijsolstr>. Wijker, Jacob Job. Spacecraft Structures. New York: Springer, 2008. Purdue University, West Lafayette, IN. 16 Feb. 2009 <http://http://www.springerlink.com/content/k4hv69/>.