| Use of statical indentation laws in the impact analysis of laminated composite plates TM Tan, CT Sun | 408 | 1985 |
| The use of stitching to suppress delamination in laminated composites LA Mignery, CT Sun, TM Tan ASTM International, 1985 | 167 | 1985 |
| An experimental study on the effect of failure trigger mechanisms on the energy absorption capability of CFRP tubes under axial compression D Siromani, G Henderson, D Mikita, K Mirarchi, R Park, J Smolko, ... Composites Part A: applied science and manufacturing 64, 25-35, 2014 | 127 | 2014 |
| Finite element modeling of the crushing behavior of thin-walled CFRP tubes under axial compression D Siromani, J Awerbuch, TM Tan Composites Part B: Engineering 64, 50-58, 2014 | 127 | 2014 |
| Wave Propagation in Graphite/Epoxy Laminate due to Impact TMIN TAN Purdue University, 1982 | 73 | 1982 |
| A Mode I cohesive law characterization procedure for through-the-thickness crack propagation in composite laminates A Bergan, C Dávila, F Leone, J Awerbuch, TM Tan Composites Part B: Engineering 94, 338-349, 2016 | 63 | 2016 |
| A crashworthiness study of a Boeing 737 fuselage section A Byar Drexel University, 2004 | 41 | 2004 |
| Wave propagation in a graphite/epoxy laminate CT Sun, TM Tan Engineering science and mechanics; International Symposium, 1983 | 31 | 1983 |
| Assessment of damage containment features of a full-scale PRSEUS fuselage panel A Bergan, J Bakuckas Jr, J Awerbuch, TM Tan Composite Structures 113, 174-185, 2014 | 28 | 2014 |
| Detecting and locating damage initiation and progression in full-scale sandwich composite fuselage panels using acoustic emission FA Leone Jr, D Ozevin, J Awerbuch, TM Tan Journal of Composite Materials 47 (13), 1643-1664, 2013 | 28 | 2013 |
| Crashworthy design and analysis of aircraft structures D Siromani Drexel University, 2013 | 21 | 2013 |
| Full-scale test and analysis of a PRSEUS fuselage panel to assess damage-containment features A Bergan, JG Bakuckas, AE Lovejoy, DC Jegley, KA Linton, G Korkosz, ... 2011 Aircraft Airworthiness and Sustainment (AAS) Conference, 2011 | 21 | 2011 |
| Computational methodology to predict damage growth in unidirectional composites—I. Theoretical formulation and numerical implementation JG Bakuckas Jr, ACW Lau, TM Tan, J Awerbuch Engineering fracture mechanics 52 (5), 937-951, 1995 | 19 | 1995 |
| Fatigue testing of a stiffened lap joint curved fuselage structure A Ahmed, JG Bakuckas Jr, J Awerbuch, AC Lau, TM Tan Journal of aircraft 44 (3), 750-757, 2007 | 18 | 2007 |
| Test and analysis of stitched composite structures to assess damage containment capability AC Bergan Drexel University, 2014 | 17 | 2014 |
| On the applicability of acoustic emission to identify modes of damage in full-scale composite fuselage structures J Awerbuch, FA Leone Jr, D Ozevin, TM Tan Journal of Composite Materials 50 (4), 447-469, 2016 | 16 | 2016 |
| Dynamic response of SMC to impact of a steel ball(Sheet Molding Compound) CT Sun, BV Sankar, TM Tan 1981 advances in aerospace structures and materials, 99-107, 1981 | 16 | 1981 |
| A modified finite element-transfer matrix for control design of space structures TM Tan, A Yousuff, LY Bahar, M Konstantinidis Computers & structures 36 (1), 47-55, 1990 | 15 | 1990 |
| Reconstruction of fatigue crack growth in AA2024-T3 and AA2198-T8 fastened lap joints D Stanley, J Awerbuch, TM Tan, B Anasori Theoretical and Applied Fracture Mechanics 82, 33-50, 2016 | 14 | 2016 |
| Acoustic emission analysis of full-scale honeycomb sandwich composite curved fuselage panels FA Leone, D Ozevin, V Godinez, B Mosinyi, JG Bakuckas, J Awerbuch, ... Nondestructive Characterization for Composite Materials, Aerospace …, 2008 | 11 | 2008 |
