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7] A FINITE ELEMENT AND EXPERIMENTAL INVESTIGATION ON THE FATIGUE OF RIVETED LAP JOINTS IN AIRCRAFT APPLICATIONS, A Dissertation Presented to The Academic Faculty, Amarendra Atre, Georgia Institute of Technology May 2006

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BIBLIOGRAFIA    

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[Rif.  5]     Federal  Aviation  Administration,  FAR  Federal  Aviation  Regulations,  Part  23.  

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[Rif.  7]     A  FINITE  ELEMENT  AND  EXPERIMENTAL  INVESTIGATION  ON  THE  FATIGUE   OF  RIVETED  LAP  JOINTS  IN  AIRCRAFT  APPLICATIONS,  A  Dissertation  

Presented  to  The  Academic  Faculty,  Amarendra  Atre,  Georgia  Institute  of   Technology  May  2006.  

[Rif.  8]     A  Practical  Guide  to  Reliable  Finite  Element  Modelling,  Alan  Morris,  Wiley,  2008.  

[Rif.  9]     Adjoint  Sensitivity  Analysis  in  MSC/NASTRAN,  Erwin  H.  Johnson,  Los  Angeles,   California.  

[Rif.  10]     AGARD  R  767,  Advisory  Group  Aerospace  Research  &  Development,  Short-­‐‑Crack   Growth  Behaviour  in  Various  Aircraft  Materials,  North  Atlantic  Treaty  Arganization.  

[Rif.  11]     Repertorio  Federate  2010,  Members  Directory,  AIAD.  

[Rif.  12]     Fastener  Modeling  for  Joining  Parts  Modeled  by  Shell  and  Solid  Elements,   Alexander  Rutman,  Chris  Boshers,  October  11-­‐‑12,  2007  Detroit,  MI  

[Rif.  13]     CALCOLO  STRUTTURALE  E  SIMULAZIONI  DI  COSTRUZIONI  INCOLLATE,   Alenia  Spazio,  G.  Augello  M.  Montabone,  Adesivi  2002,  Reggio  Emilia,  24  Giugno   2002.  

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[Rif.  14]     Aluminium  Design  and  Construction,  John  Dwight,  University  of  Cambridge;  and   Fellow  of  Magdalene  College,  Cambridge,  1999.  

[Rif.  15]     An  Evaluation  of  Common  Analysis  Methods  for  Bolted  Joints  in  Launch  Vehicles,   Grant  M.  Henson_  and  Bryes  A.  Hornish,  Structural  Dynamics,  and  Materials   Conference<BR>18th,  12  -­‐‑  15  April  2010,  Orlando,  Florida.  

[Rif.  16]     ANALISI  DEL  COMPORTAMENTO  DAMAGE  TOLERANT  DI  UN  PANNELLO   SANDWICH,  M.  Giglio,  A.  Manes,  Dipartimento  di  Meccanica,  Politecnico  di   Milano,  XVIII  Convegno  Nazionale  IGF  Cetraro  (CS),  31  Maggio  –  1  Giugno  2006.  

[Rif.  17]     Analisi  FEM  di  velivoli  HALE-­‐‑UAV  ad  energia  solare  e  modelli  di  predizione  del   peso  strutturale,  Luca  Montanelli,  Università  di  Pisa,  Tesi  di  Laurea  Specialistica.  

[Rif.  18]     Analysis  of  Fasteners  as  Disbond  Arrest  Mechanism  for  Laminated  Composite   Structures,  Chi  Ho  E.  Cheung,  Phillip  M.  Gray,  Gerald  E.  Mabson  and  Kuen  Y.  Lin,   University  of  Washington,  Seattle,  WA,  98195-­‐‑2400.  

[Rif.  19]     Computational  Approaches  for  Aerospace  Design,  The  pursuit  of  Excellence,  Andy  J.  

Keane  Prasanth  B.  Nair,  University  of  Southampton,  John  Wiley  &  Sons,  Ltd,  2005.  

[Rif.  20]     DAMAGE  TOLERANCE  IN  PRESSURIZED  FUSELAGES,  T.  Swift.    

[Rif.  21]     Dimensionamento  strutturale  effettuato  con  le  norme  CE  94/25  e  confronto   attraverso  il  metodo  degli  elementi  finiti,  Ing.  Vittorio  BOCCOLINI,  Tesi  di   dottorato,  Università  degli  Studi  Federico  II  di  Napoli.  

[Rif.  22]     Engineering  Fundamentals  of  Threaded  Fastener  Design  and  Analysis,  Ralph  S.  

Shoberg,  P.E.,  Director  of  Technology,  PCB  Load  &  Torque,  Inc,  ISO9001Certified   A2LA  Accredited  to  ISO17025.  

[Rif.  23]     Fastener  Modeling  for  Joining  Composite  Parts,  Alexander  Rutman,  Chris  Boshers  –   Spirit  AeroSystems  Larry  Pearce,  John  Parady  –  MSC.Software  Corporation,  2009   Americas  Virtual  Product  Development  Conference  April  21-­‐‑22,  2009  Phoenix,  AZ.  

[Rif.  24]     Fastener  Modeling  for  Joining  Parts  Modeled  by  Shell  and  Solid  Elements,  

Alexander  Rutman,  Chris  Boshers  –  Spirit  AeroSystems  Larry  Pearce,  John  Parady  –   MSC.Software  Corporation,  2007  Americas  Virtual  Product  Development  

Conference  October  11-­‐‑12,  2007  Detroit,  MI.  

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[Rif.  25]     INTRODUCTION  to  FINITE  ELEMENT  METHODS,  Carlos  A.  Felippa,  Department   of  Aerospace  Engineering  Sciences  and  Center  for  Aerospace  Structures  University   of  Colorado  Boulder,  Colorado  80309-­‐‑0429,  USA.  

[Rif.  26]     EARLY  FINITE  ELEMENT  RESEARCH  AT  BERKELEY,  Ray  W.  Clough,  Edward  L.  

Wilson,  Present  at  the  Fifth  U.S.  National  Conference  on  Computational  Mechanics,   Aug.  4-­‐‑6,  1999.  

[Rif.  27]     FINITE  ELEMENT  ANALYSES  OF  A  LAMINATED  BLADE  RETENTION  SYSTEM,   Dennis  K.  McCarthy,  Robert  T.  Fort,  McDonnell  Douglas  Helicopter  Systems  5000   East  McDowell  Mesa,  Arizona  85215.  

[Rif.  28]     Guide  to  Design  Criteria  for  Bolted  and  Riveted  Joints,  Second  Edition,  Geoffrey  L.  

Kulak,  John  W.  Fisher,  John  H.  A.  Struik,  AMERICAN  INSTITUTE  OF  STEEL   CONSTRUCTION,  Inc.  One  East  Wacker  Drive,  Suite  3100,  Chicago,  IL  60601.  

[Rif.  29]     Langley  Integrated  Design  Center  (IDC)  Procedures:  Discipline  Processes  and   Interfaces  between  Stations,  NASA  Langley  IDC  Operating  Manual,  Discipline   Interfaces  7/14/2011.  

[Rif.  30]   Link  Mesh  Model  of  Elementary  Panel  Bay  for  Linear  MSC/NASTRAN/Parametric   Analysis  of  Stiffened  Shells,  Steven  Basic,  Boeing  Commercial  Airplane  Group  777-­‐‑

300,  Structures  Technology,  3801  South  Oliver,  MS  K95-­‐‑04,  Wichita,  KS  67210.  

[Rif.  31]     MSC  Aerospace  Solutions:  Optimizing  the  Design-­‐‑to-­‐‑Certification  Process,   Aerospace  Business  Unit  The  MacNeal-­‐‑Schwendler  Corporation  Los  Angeles,   California  USA.  

[Rif.  32]   MULTI-­‐‑SPRING  REPRESENTATION  OF  FASTENERS  FOR  MSC/NASTRAN   MODELING,  Alexander  Rutman,  Ph.  D,  Joseph  Bales-­‐‑Kogan,  M.  Sc.,  Boeing   Commercial  Airplane  Group  Strut  Structures  Technology  MS  K95-­‐‑04  3801  South   Oliver,  Wichita,  Kansas  67210.  

[Rif.  33]     Nonlinear  Strenght  and  Stability  Analysis  of  Landing  Gear  Componet,  Andrew   Mera,  The  Boeing  Co.  Information,  Space  and  Defense  Systems  Group,  Seattle,  WA.  

[Rif.  34]   Prediction  of  Optimum  Spectrum  for  Full  Scale  Fatigue  Test,  C.M.  Manjunatha  and   V.R.  Ranganath,  Structural  Integrity  Division,  National  Aerospace  Laboratories,   Bangalore-­‐‑560  017,  India.  

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[Rif.  35]   Progettazione  di  Strutture  Aerospaziali  II,  Daniele  Fanteria  ,  Dia  Dipartimento   Ingegneria  Aerospaziale,  Università  di  Pisa.  

[Rif.  36]   Progettazione  di  Strutture  Aerospaziali  ,  Giuseppe  Quaranta,  Polimi.  

[Rif.  37]   Progettodellastrutturadi  supportodel  sistemadi  propulsioneper  il  satellite   Microscope,  ANALISI  MECCANICHE.  

[Rif.  38]     Residual  Strength  Analyses  of  Riveted  Lap-­‐‑Splice  Joints,  B.  R.  Seshadri  and  J.  C.  

Newman,  Jr.  Langley  Research  Center,  NASA/TM-­‐‑2000-­‐‑209856,    Hampton,  Virginia.  

[Rif.  39]     Specification  for  Structural  Joints  Using  High-­‐‑Strength  Bolts,  RCSC,  December  31,   2009.  

[Rif.  40]   Stress  Concentration  Factor  Determination  for  Various  Tensile  Test  Specimen   Configurations  by  the  Finite  Element  Method  using  MSC/PATRAN  and  

MSC/NASTRAN,  Dr.  Gregory  A.  Shoales,  P.E.  Lt  Col  Scott  A.  Fawaz,  Ph.D.,  P.E.,   USAF,  Center  for  Aircraft  Structural  Life  Extension  (CAStLE)  Department  of   Engineering  Mechanics,  February  2004,  USAFA  TR  04-­‐‑03.  

[Rif.  41]   STRUCTURAL  ANALYSIS  FOR  THE  21ST  CENTURY,  Brian  P.  Oldfield,   Technologist  Advisor,  British  Aerospace,  Military  Aircraft  and  Aerostructures   Warton  Aerodrome,  Preston,  Lancashire.  

[Rif.  42]   Modello  FEM  dell’ala  di  un  velivolo  dell’Aviazione  Generale,  correlazione   numerico-­‐‑  sperimentale,  Cristian  Valles,  Tesi  di  laurea,  FACOLTA’  DI  

INGEGNERIA  CORSO  DI  LAUREA  IN  INGEGNERIA  AEROSPAZIALE,  Università   Di  Napoli.  

[Rif.  43]   Valutazioni  teoriche,  numeriche  e  sperimentali  delle  proprietà  di  trasmissione   sonora  (Trasmission  Loss)  di  pannelli  piani,  Ing.  Fabio  Russo,  DOTTORATO  DI   RICERCA  IN  INGEGNERIA  AEROSPAZIALE,  Università  Di  Napoli.  

[Rif.  44]   VERIFICHE  STATICHE  DELLE  STRUTTURE  PRIMARIE  DI  UN  ALIANTE  DI   CLASSE  CLUB,  Claudio  BALESTRI,  Massimiliano  PRESOTTO,  Lavoro  di  Tesi,   Facoltà  di  Ingegneria  Dipartimento  di  Ingegneria  Aerospaziale,  POLITECNICO  DI   MILANO.  

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[Rif.  45]   An  investisgation  on  Fatigue  of  Fuselage  Riveted  Lap  Joints,  Load  Transfer  in   Riveted  Lap  Joint,  Chapter  7.  

[Rif.  46]   Fatigue  of  Mechanically  Fastened  Joints,  Harold  Reemsnyder,  Bethlehem  Steel   Corporation,  Influence  of  Fastener  Flexibility  on  the  Prediction  of  Load  Transfer  and   Fatigue  Life  for  Multiple-­‐‑Row  Joints,  Heimo  Huth.  

   

 

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