RICERCA ITALIANA     

Programmi di ricerca simili:

• 1 - MONITORAGGIO DELL'INTEGRITA' STRUTTURALE DELLE COSTRUZIONI AEROSPAZIALI
• 2 - Problemi e modelli microstrutturali: applicazioni in ingegneria strutturale e civile
• 3 - Problemi multi-scala con interazioni complesse nell’ingegneria strutturale
• 4 - Sviluppo e applicazione di procedure ibride numerico-sperimentali basate su tecniche ottiche per la caratterizzazione di materiali innovativi per uso industriale e biomedico.
• 5 - Strutture in materiali con microstruttura. Una sfida per la moderna ingegneria civile.
• 6 - Resistenza e degrado di interfacce in materiali e sistemi strutturali
• 7 - Comportamento dinamico di strutture in campo lineare e nonlineare: dalla modellazione alla sperimentazione
• 8 - Collegamenti strutturali, discontinuita' fisiche e interfacce materiali: analisi e sperimentazione.
• 9 - Tecniche e materiali innovativi per il rinforzo sismico di strutture esistenti
• 10 - Diagnostica e salvaguardia di opere in calcestruzzo armato per le infrastrutture con degrado ambientale.

Classificazione scientifico-disciplinare

• Area scientifico disciplinare: Ingegneria industriale e dell'informazione
  • COSTRUZIONI E STRUTTURE AEROSPAZIALI
  • FLUIDODINAMICA
  • DISEGNO E METODI DELL'INGEGNERIA INDUSTRIALE
  • TECNOLOGIE E SISTEMI DI LAVORAZIONE
  • SCIENZA E TECNOLOGIA DEI MATERIALI

Classificazione brevettuale

• HUMAN NECESSITIES
  • MEDICAL OR VETERINARY SCIENCE; HYGIENE
    • FILTERS IMPLANTABLE INTO BLOOD VESSELS; PROSTHESES; ORTHOPAEDIC, NURSING OR CONTRACEPTIVE DEVICES; FOMENTATION; TREATMENT OR PROTECTION OF EYES OR EARS; BANDAGES, DRESSINGS OR ABSORBENT PADS; FIRST-AID KITS (dental prosthetics A61C)

Classificazione geografica

• Regione: Campania

Bibliografia

[1] R. M. Jones “Mechanics of Composite Materials”, Taylor & Francis 1998
[2] L. Ilcewicz, Material Qualification/Equivalency Protocol and Acceptance Criteria for Shared Database, NASA/AGATE CMQE Workshop, Kansas, September 2000
[3] T. Smith, J. Tomblin, et alii, Material Qualification methodology for Epoxy Based Prepreg Composite Material Systems, NASA/AGATE, Aircraft Certification Service of FAA- USA February 1999
[4] “Design of a composite wing extension for a general aviation aircraft” NASA report CR 173832
[5] G. L. Giles, “Design Oriented Analysis of Aircraft Fuselage Structures”, NASA report 1992
[6] Jérôme Pora, Composite Materials in the Airbus A380, Large Aircraft Division, AIRBUS FRANCE, ICCM 13th – Beijing, June 2001
[7] B. Rackers, The Challenge for Advanced Composites to Increase Applications on Commercial Aircraft, AIRBUS GMBH, ICCM 13th – Beijing, June 2001
[8] E. D. (Dave) Ledbetter, Future Composite Research and Development Programs to Support Aerospace Needs, LOCKHEED MARTIN AERONAUTICS CO., ICCM 13th – Beijing, June 2001
[9] S. Abrate, “Impact on laminated composite materials”, Applied Mechanics Review, Vol.44, N.4, pp.150-190, 1991
[10] W. J. Cantwell, J. Morton, “The impact resistance of composite materials – a review”, Composites, Vol. 22, pp. 347-362, 1991
[11] E. J. Herup, “Low-velocity impact on composite sandwich plates, PhD Thesis, AIR Force Institute of Technology Wright-Patterson AFB OH, 1996
[12] K. N. Shivakumar, W. Elberg, W. Illg, “Prediction of impact force and duration due to low-velocity impact on circular composite plates”, Journal of Applied Mechanics, Vol. 52, pp. 654-680, 1985
[13] A. K. Noor, “Structure Technology for Future Aerospace Systems”, American Institute of Aeronautics and Astronautics, 2000
[14] M. H. Aliabadi, “Boundary Element Formulations in Fracture Mechanics”, Appl.Mech. Rev. Vol. 50, No. 2, February 1997
[15] N. Salgano “Boundary Element methods for Damage Tolerance Design of Aircraft Structures”, Computational Mechanics Publications, 1998
[16] Accardo, A. F., Ricci, F., Basso, P., , "Design and Development of Low Altitude Unmanned Aerial Vehicle", Harrogate UK, 22nd International Congress of Aeronautical Science ICAS 2000
[17] Accardo, A. F., Ricci, F., Basso, P., , "Design, Realization and Testing of an Advanced Composite Unmanned Aircraft", 13th International Conference on Composite Materials (ICCM13th), June 2001- Beijing CINA
[18] Accardo, A. F., Ricci, F., Basso, “Application of advanced composite materials for Unmanned Vehicles”, ECCM10 European Conference on Composite Materials, June 2002 Bruges Belgium
[19] Boeing Design Manual, 1985
[20] Boeing Specification Support, 1998
[21] ASTM, American Standard Test Methods, 1996
[22] MIL HDBK 17E - USA, 23 January 1997
[23] Proceedings of the Second CEAS-ACS Workshop on Aircraft Interior Noise Control, Friedrichshafen, June 8th 1998
[24] Proceedings of the 5th AIAA/CEAS Aeroacoustics conference, Bellevue (Greater Seattle)10 -12 May 1999
[25] David G. Stephens and F. W. Cazier jr, " NASA Noise reduction Program for advanced subsonic transports», Noise Control Engineering. J.44(3), 1996
[26] "Vibro-Acoustic modal testing at NASA Langley research center". Richard S. Pappa, Jocelyn I. Pritchard , Ralph D. Buehrle. - NASA/TM -1999 -209319 ARL-TR-1980
[27] AA. VV., (tra cui F. Marulo, S. De Rosa) Aeroacoustics Research in Europe: The CEAS-ASC Report on 1997 Highlights, Aerotecnica Missili & Spazio, Vol. 77, n.ri 1-2, Jan – Jun, 1998.
[28] K. A. Cunefare, S.De Rosa, An Improved State-Space Method for Coupled Fluid-Structure Interaction Analysis, Journal of Acoustical Society of America, Vol.105(1), January 1999, pp.206-210.
[29] K. A. Cunefare, S.De Rosa, The Sensitivity of Structural Acoustic Response to Attachment Feature Scale Representation, Journal of Acoustical Society of America, Vol.106(6), December 1999, pp.3384-3393.
[30] S.De Rosa, F.Franco, F.Marulo, G.Esposito, F.Conicella, Full Validation of the Structural-Acoustic Response of a Simple Enclosure, Journal of Aircraft, AIAA Series, Vol.36(5), Sep-Oct 1999, pp.866-875.
[31] E.Monaco, F.Franco and L.Lecce, Experimental and numerical activities on damage detection using magnetostrictive actuators and statistical analysis, Journal of Intelligent Material System and Structures", Vol. 11, July 2000, pp. 567-578
[32] S.De Rosa, F.Franco, M.Fontana , R.Paino, A.Paonessa, A.Sollo, The Structural Acoustic Optimisation of a Cylinder Model with the Finite Element Method, 2nd CEAS-ASC Workshop on Aircraft Interior Noise Control, June 8-9, Daimler-Benz Aerospace Dornier, Friedrichshafen, Germany.
[33] A.Sollo, S.De Rosa, F.Franco, M.Fontana, R.Paino, The Structural Acoustic Optimisation of a Stiffened Cylinder Model, Proceed. of the 25th MSC/NASTRAN Italian Users' Conference, October15-16, Torino, Italy. paper n.25.
[34] Sollo, A., Lecce, L., Quaranta, V., Doelman, N., Doppemberg, E., Active Noise Control on ATR Fuselage Mock-Up by Piezoceramic Actuators, 4th AIAA/CEAS Aeroacoustic Conference,Toulouse, June 2-4, 1998, AIAA paper –98-2230, pp. 174-183.
[35] Lecce, L., Franco, F., Results and Prospects for the Project MADAVIC (Magnetostrictive Actuators for Damage Analysis and Vibration Control), ACTUATOR 98- 6th Intern. Conference on New Actuators, 17-19 june 1998, Bremen, Germany, pp. 389-394.
[36] F. Marulo, P. Cascone, C. Ntounas, A. Sollo, A. Pezzolla, Un Codice per il Calcolo Semplificato del Rumore Interno, XV Congresso Nazionale AIDAA, Torino, 15-19 Novembre 1999.
[37] F. Marulo, N. De Guida, Prime Esperienze di Misura con il Tubo ad Impedenza a Due Microfoni, XV Congresso Nazionale AIDAA, Torino, 15-19 Novembre 1999.
[38] Paonessa A., Napolitano L., Melluso D., Marulo F., Simulazione numerica di trattamento viscoelastico su pannelli di fusoliera, XVII Congresso Nazionale AIDAA, Roma, 15-19 Settembre 2003 .
[39] F.Ricci, E.Monaco, T.Polito, F.Marulo, Influence of experimental testing set-up and geometric parameters on damping measurements, SPIE 11th Annual International Symposium on Smart Structures and Materials, San Diego, CA USA , 14-18 March 2004

Parole Chiave

FUSOLIERE PRESSURIZZATE; MATERIALI COMPOSITI; MONITORAGGIO INTEGRITÀ STRUTTURALE; FATICA; MODELLAZIONE STRUTTURALE; VERIFICA STRUTTURALE SPERIMENTALE; MATERIALI INTELLIGENTI; TECNICHE DI LAVORAZIONE; EFFICIENZA STRUTTURALE