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NASA Glenn Research Center, Cleveland, Ohio
A notice written for the news report: “SAE Update (News for the Members of SAE)”, Vol. 20, No. 4, April 2003, about Dr. Chamis becoming a Fellow of SAE (SAE = Society of Automotive/Aerospace Engineers):
Christos C. Chamis, Senior Aerospace Scientist, NASA Glenn Research Center, for his pioneering contributions to the field of science and engineering in 3-D inelastic analysis, probabilistic structural analysis, structural tailoring, and high-temperature composite mechanics in which he developed computational methods and computer codes.
Christos C. Chamis, “Polymer Composite Mechanics Review — 1965 to 2006”, Journal of Reinforced Plastics and Composites, July 2007, vol. 26, no. 10, pp. 987-1019,
doi: 10.1177/0731684407079419
C.C. Chamis, Design oriented analysis and structural synthesis of multilayered filamentary composites, Ph.D. thesis, Case Western Reserve University, Cleveland, Ohio, 1967
Chamis CC, Sendeckyj GP. Critique on theories predicting thermo-elastic properties of fibrous composites. J Compos Mater 1968;2(3):332–58.
Chamis, C. C., Buckling of Anisotropic Composite Plates, ASCE, pp. 2119-2139, October 1969.
C. C. Chamis, “Buckling of anisotropic composite plates”, ASCE J. Structural Div., Vol. 95, No. ST10, October 1969, pp. 2119-2139
Chamis C.C., 1969, Failure criteria for filamentary composites, Composite Materials: Testing and Design, ASTM STP 460: 336-351.
Christos C. Chamis, “Characterization and design mechanics for fiber-reinforced metals”, NASA TN D-5784, 1970
Christos C. Chamis, “Design and Analysis of Fiber Composite Structural Components”, Aerospace Structural Materials. NASA SP-227, 330 pages, published by NASA, Washington, D.C., 1970, p.217
Chamis, C. C., Buckling of Boron/Aluminum and Graphite/Resin Fiber Composite Anisotropic Panels, Natl. Sampe Conf. on Space Shuttle Materials, 1971.
Chamis, C. C., Theoretical Buckling Loads of Boron/Aluminum and Graphite/Resin Fiber Composite Anisotropic Plates, NASA TN D6572, December 1971.
Christos C. Chamis (NASA Lewis Research Center), “Computer Code for the Analysis of Multilayered Fiber Composites. Users Manual”, NASA Technical note TN D-7013, Accession No. A053503, March 1971
Christos C. Chamis (NASA Lewis Research Center, Cleveland, Ohio), “Theoretical Buckling Loads of Boron/Aluminum and Graphite/Resin Fiber-Composite Anisotropic Plates.”, NASA Technical Note TN D-6572, December 1971
C.C. Chamis (NASA Lewis Research Center, Cleveland, Ohio), “Residual stresses in angleplied laminates and their effects on laminate behavior”, Metallurgical Society of AIME, International Conference on Composite Materials, 2nd, Toronto, Canada; United States; 16-20 Apr. 1978. 23 pp. 1978
C. C. Chamis and G. T. Smith, 'Composite Durability Structural Analysis," NASA TM-79070, 1978.
Sinclair, J.H. and Chamis, C.C., "Compressive Behavior of Unidirectional Fibrous Composites," Compression Testing of Homogeneous Materials and Composites, STP 808, American Society for Testing and Materials, Philadelphia, PA, 1983.
Chamis, C.C. Simplified composites micromechanics equations for strength, fracture toughness, and environmental effects. NASA TM-83696, USA, 1984
Caruso, J.J. and C.C. Chamis, “Assessment of Simplified Composite Micromechanics Using Three-Dimensional Finite-Element Analysis”, J. Compos. Technol. Res., Vol/Issue 8, 1986, pp. 77- 83
Christos C. Chamis, “Probabilistic structural analysis methods for space propulsion system components”, Probabilistic Engineering Mechanics, Vol. 2, No.2, June 1987, pp. 100-110, doi:10.1016/0266-8920(87)90021-X
P. L. N. Murthy and C. C. Chamis, Integrated Composite Analyzer (ICAN): Users and Programmers Manual, NASA Technical Paper 2515, March 1986.
L. Minnetyan, C. C. Chamis, and P. L. N. Murthy, "Structural Behavior of Composites with Progressive Fracture," NASA TM-102370, January 1990, 18 pp.
For more see the link: Dr. Christos C. Chamis
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