NISA in Cutting-Edge Applications

Space Applications

1. Development of a non destructive vibration technique for bond assessment of space shuttle tiles. - Dr.Faissal A.Moslehy, P.E
2. Design Tool For Inflatable Space Structures - Arthur L. Palisoc and Yuli Huang (L’Garde, Inc.Tustin, California)
3. Rapid Modeling and Analysis Tools- Norman F.Knight and Thomas J.Stone Veridian Systems Division,Chantilly , Virginia
4. Analysis and design of a moment sensitive flexure jointed Stewart Platform based force-torque sensor- Mulgundmath Prashanth, Shivanand Bhavikatti, R. Ranganath, and A. Ghosal

Nuclear Applications

1. Finite element stress analysis of spent nuclear fuel disposal canister in a deep geological repository-KWON Young Joo ; CHOI Jong Won (Department of Mechano-Informatics & Design Engineering, Hongik University, 34 Shinanri, Chochiwoneup, Yeonki-gun, Choongnam 339-701, COREE, REPUBLIQUE DE Korea Atomic Energy Research Institute, COREE, REPUBLIQUE DE)
2. Seismic design considerations of nuclear fuel cycle facilities

Composites

1. LIGHTWEIGHT CONSTRUCTION FOR ADVANCED SHIPBUILDING – RECENT DEVELOPMENT- P. Noury*, B. Hayman, D. McGeorge and J. Weitzenböck
2. Carbon fiber/epoxy wheels developed to replace metal wheels on large freight trailers Semi-trailers roll lighter with Prins Dokkum\'s carbon fiber Dynawheels- Dale Brosius, Contributing Writer Composites Technology
3. Linear static analysis of composite hat-stiffened laminated shells using finite elements- B. Gangadhara Prusty  Department of Maritime Engineering, Australian Maritime College, Launceston-7250, Australia
4. Effects of Battle Damage Repair on the Natural Frequencies and Mode Shapes of Curved Rectangular Composite Panels.- Goodwin, William P.
5. Sandwich plates-free vibrations and damping analysis- A. Muc and P. Zuchara
6. Orbital Stress Analysis—Part I: Simulation of Orbital Deformation Following Blunt Injury by Finite Element Analysis Method-Jehad Al-Sukhun PhD, MSc, BDS
7. A new approach to static and dynamic analysis of composite plates with different boundary conditions-M. R. Khalili, K. Malekzadeh and R. K. Mittal
8. Classical coupled thermoelasticity in laminated composite plates based on third-order shear deformation theory-Kamran Daneshjo and Morteza Ramezani(Department of Mechanical Engineering, Iran University of Science and Technology, P.O. Box 16844, Narmak, Tehran, Iran)
9. Wing instability of a full composite aircraft-Mahmood M. Shokrieh and Fathollah Taheri Behrooz (Mechanical Engineering Department, Iran University of Science and Technology, Narmak, Tehran 16844, Iran)
10. Coupled thermoelasticity in laminated composite plates based on Green–Lindsay model-Kamran Daneshjoo and Morteza Ramezan (Mechanical Engineering Department, Iran University of Science and Technology, Narmak, Tehran, Iran
    Structural Department of Advanced Electronic Research Center, Pasdaran, Tehran, Iran)
11. Classical coupled thermoelasticity in laminated composite plates based on third-order shear deformation theory-Kamran Daneshjo and Morteza Ramezani(Department of Mechanical Engineering, Iran University of Science and Technology, P.O. Box 16844, Narmak, Tehran, Iran)
12. Free Vibrational Responses of FRP Composite Plates: Experimental and Numerical Studies-S. Chakraborty M. Mukhopadhyay (Department of Mechanical Engineering, Indian Institute of Technology, Kharagpur, 721302, India)
13. Optimum design of composite laminates with STROPT-S. Belsare, M. HaririanEngineering Mechanics Research Corporation, 1607 East Big Beaver Road, Troy, Michigan, U.S.A.
14. NON-LINEAR ANALYSIS WITH AN AXISYMMETRIC THICK SHELL ELEMENT-R. V. RAVICHANDRAN ^*, A. VENKATESH (Engineering Mechanics Research Corporation, P.O. Box 696, Troy, MI 48099, U.S.A.)
15. Sensing of delamination in laminated composite beams using multiple magnetostrictive patches-Eslavath, Saidha and Naik, Narayana G and Gopalakrishnan, S and Kumar, M (2003) Sensing of delamination in laminated composite beams using multiple magnetostrictive patches. In Mohan, S and Dattaguru, B and Gopalakrishnan, S,( Eds. Proceedings SPIE: Smart Materials, Structures, and Systems, pages Vol.5062, 691-699, Bangalore, India.)
16. Towards a Rational Failure Criterion for Unidirectional Composite Laminae-A. V. Krishna Murty ;  G. Narayana Naik a; S. Gopalakrishnan (Department of Aerospace Engineering, Indian Institute of Science, Bangalore, India)
17. Sandwich plates-free vibrations and damping analysis-A. Muc and P. Zuchara
18. ADHESIVE BONDING TECHNOLOGIES FOR AUTOMOTIVESTRUCTURAL COMPOSITES-OAK RIDGE NATIONAL LABORATORY
19. Effects of Stacking Sequence on theImpact Damage Resistance of Composite Laminates-Edgar Fuoss B. A. Sc. (Enginee~gP hysics) (Department of Mechanical and Aerospace Engineering The Ottawa-Carleton Institute for Mechanical and Aerospace Engineering Carleton University Ottawa, Ontario, Canada)
20. Buckling and failure analysis of FRP faced sandwich plates-A. Muc and P. Zuchara (Institute of Mechanics and Machine Design, Cracow University of Technology, ul. Warszawska 24, 31-155, Kraków, Poland)
21. Optimum Design and development of a scost effective pultruded hybrid composite mast- Mahir Hassan ( Dalhousie University-Daltech)
22. Application of Differential Quadrature Mechod to the Analysis of Delamination Buckling of Laminated Composites-Shapour Moradi ( Dalhousie University-Daltech)

Aerospace Applications:

1. Correlation/Validation of Finite Element Code Analyses for Vibration Assessment of Avionic Equipment.- Bhungalla, Amar ; Kurylowich, George (WRIGHT RESEARCH AND DEVELOPMENT CENTER WRIGHT-PATTERSON AFB OH)
2. Structural and Vibrational Analysis of a PlastIc Annular Wind Tunnel Parachute Model-Benney, Richard J (ARMY NATICK RESEARCH DEVELOPMENT AND ENGINEERING CENTER MA)
3. Finite Element Analysis of a Rudder-Harish Mukundan (Department of Ocean Engineering Indian Institute of Technology, Madras)
4. FAA-NASA Symposium on the Continued Airworthiness of Aircraft Structures -FAA Center of Excellence in Computational Modeling of Aircraft StructuresAtlanta, Georgia

General

1. Experimental and finite element prediction of bursting pressure in compound cylinders-G.H. Majzoobi, G.H. Farrahi, M.K. Pipelzadeh and A. Akbari(Faculty of Engineering, Bu- Ali Sina university, Hamadan, Iran)
2. An incremental approach for large displacement response of structures subjected to dynamic loads - V. Ramamurti, S. Rajarajan and G. Venkateswara Rao
3. Vibration Energy Flow Analysis in Randomly Parametered Coupled Plate Structures using Green’s Function Coupling Technique
4. Experimental comparison of dynamic FEA results of a permanent magnet brushless DC linear motor- G. Abdou; W. Tereshkovich
5. Finite Element Analysis and Reliability Assessment of Spherical LPG Storage Tank- K Ramaneyulu, A Husain, Dr D K Sehgal, Dr S Ahmad
6. Simulation for Compressive Behavior of Cartons-Hironobu Hirano, Takao Kobayashi and Isao Kodaka(Pulp and Paper Research Lab. Oji Paper Co., Ltd.)
7. RESIDUAL STRESSES DUE TO WELDING OF A NOZZLE TO A PRESSURE VESSEL- Linda Karlsson
8. Reconstruction of Orbital Wall Fracture An experimental and clinical study- Risto Kontio (Departments of Oral and Maxillofacial Surgery Helsinki University Central Hospital )
9. Orbital stress analysis--Part I: Simulation of orbital deformation following blunt injury by finite element analysis method.- Al-Sukhun J, Kontio R, Lindqvist C.( Department of Oral and Maxillofacial Surgery, Helsinki University Central Hospital, Kasarmikatu 11-13, PO Box 263, 00029 HUS, Helsinki, Finland.)
10. Thermal stress analysis of the parting plane flange joint of an industrial steam turbine- R S ALWAR¹, S SRINIVASARAO² (¹ Indian Institute of Technology, Madras, India ² BHEL, Hyderabad, India)

Disclaimer: Most of the articles listed are hosted on other Websites. You may be required to register, activate a subscription or purchase the article before you can obtain the full text.