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Joseph F. Rakow, Ph.D. - Publications

Affiliations: 
2005 University of Michigan, Ann Arbor, Ann Arbor, MI 
Area:
Aerospace Engineering, Mechanical Engineering
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8 high-probability publications. We are testing a new system for linking publications to authors. You can help! If you notice any inaccuracies, please sign in and mark papers as correct or incorrect matches. If you identify any major omissions or other inaccuracies in the publication list, please let us know.

Year Citation  Score
2009 Rakow JF, Pettinger AM. Failure analysis of composites: Sandwich structures Advanced Materials and Processes. 167: 24-26.  0.307
2007 Rakow JF, Waas AM. Response of actively cooled metal foam sandwich panels exposed to thermal loading Aiaa Journal. 45: 329-336. DOI: 10.2514/1.24813  0.619
2005 Rakow JF, Waas AM. Thermal buckling of metal foam sandwich panels for convective thermal protection systems Journal of Spacecraft and Rockets. 42: 832-844. DOI: 10.2514/1.9741  0.601
2005 Rakow JF, Waas AM. Size effects and the shear response of aluminum foam Mechanics of Materials. 37: 69-82. DOI: 10.1016/J.Mechmat.2003.12.002  0.549
2005 Rakow JF, Waas AM. Thermomechanical response of actively cooled metal foam sandwich panels for thermal protection systems Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 3: 1895-1917.  0.626
2004 Rakow JF, Waas AM. The Effective Isotropic Moduli of Random Fibrous Composites, Platelet Composites, and Foamed Solids Mechanics of Advanced Materials and Structures. 11: 151-173. DOI: 10.1080/15376490490277286  0.497
2004 Rakow JF, Waas AM. Thermal buckling of metal foam sandwich panels for actively cooled thermal protection systems Collection of Technical Papers - Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics and Materials Conference. 3: 2206-2221.  0.622
2003 Rakow JF, Waas AM. Size effects in metal foam cores for sandwich structures 44th Aiaa/Asme/Asce/Ahs/Asc Structures, Structural Dynamics, and Materials Conference. DOI: 10.2514/1.4839  0.586
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