Link to Index Page

Dr. John T. Wang

NASA Langley Research Center, Hampton, Virginia

Selected Publications:
Raju, I.S. and Wang, J.T., ‘Classical laminate theory models for woven fabric composites', J. Composite Tech. Res. 16(4), October (1994).
Wang, J. T., Dávila, C. G., Sleight, D. W., and Krishnamurthy, T., "Crown Panel Stiffener-Frame Intersection Structural Integrity Analyses," presented at the 5th NASA/DoD Conference on Advanced Composites Technology, Seattle, WA, 1994.
Wang, J. T., Raju, I. S., and Sleight, D. W., “Fracture Mechanics Analysis of Composite Skin-Stiffener Debond Configurations with Shell Elements,” AIAA Paper 94-1389, Proceedings, AIAA/ASME/ASCE/AHS/ASC 35th Structures, Structural Dynamics, and Materials Conference, Hilton Head, SC, April 18-20, 1994, AIAA, Washington, DC, 1994, pp. 676-693
David W. Sleight and John T. Wang, “Buckling Analysis of Debonded Sandwich Panel Under Compression”, NASA Technical Memorandum 4701, December 1995
Wang, J. T. and A. R. Johnson (2002). Deployment simulation of ultra-lightweight inflatable structures. AIAA 1261, NASA Langley Research Center.
Alexander Tessler, David W. Sleight, & John T. Wang, “Nonlinear shell modeling of thin membranes with emphasis on structural wrinkling”, 44th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference and Exhibit. Norfolk, VA: AIAA-2003-1931, 2003
Wang, J. T. 2004. Simulation nonlinear deformation of solar sail membranes using explicit time integration. 45th AIAA/ASME/ASCE Structures, Structures Dynamics, and Material Conference. April 19–22, 2004, Palm Springs, CA, USA
Alexander Tessler, David W. Sleight and John T. Wang, “Effective modeling strategies for nonlinear shell analysis of thin membranes exhibiting structural wrinkling”, Journal of Spacecraft and Rockets, Vol. 41, No. 5, September-October 2004
Tessler, A., Sleight, D. W. and Wang, J. T., 2005. Effective modeling and nonlinear shell analysis of thin membranes exhibiting structural wrinkling, Journal of Spacecraft and Rockets, 42, 2, 287–298.
Sleight, D. W., Michii, Y., Lichodziejewski, D., Derbès, B., Mann, T. O., Slade, K. N., & Wang, J. T. (2005). Finite element analysis and test-correlation of a 10 meter inflation-deployed solar sail. Structures, Structural Dynamics and Materials Conference. Austin, Texas: 46th AIAA/ASME/ASCE/AHS/ASC
John T. Wang, Clarence C. Poe, Jr., Damodar R. Ambur and David W. Sleight, “Residual strength prediction of damaged composite fuselage panel with R-curve method”, Composites Science and Technology, Vol. 66, No. 14, November 2006, pp. 2557-2565
Alexander Tessler, David W. Sleight and (possibly) John T. Wang, “Geometrically nonlinear shell analysis of wrinkled thin-film membranes with stress concentrations, NASA Technical Reports Server (NTRS), 2013

Page 123 / 250