{"id":1719,"date":"2016-10-31T03:25:53","date_gmt":"2016-10-31T03:25:53","guid":{"rendered":"https:\/\/asidiconference.org\/?page_id=1719"},"modified":"2016-10-31T03:57:50","modified_gmt":"2016-10-31T03:57:50","slug":"asidic-2012-technical-program","status":"publish","type":"page","link":"https:\/\/asidiconference.org\/?page_id=1719","title":{"rendered":"ASIDIC 2012: Technical Program"},"content":{"rendered":"

Day 1 – NOVEMBER 6th 2012
\n| National CENTER FOR AVIATION TRAINING |<\/h2>\n

Technical Session 1A: Crashworthiness of<\/span>
\nComposites & Metallic Aerospace Structures<\/span><\/h2>\n

7:00<\/strong> Breakfast & Registration<\/p>\n

8:00<\/strong> Welcome and Introductions \u2013<\/em>
\nGerardo Olivares,
\nNational Institute for Aviation Research<\/span><\/p>\n

8:10<\/strong> Keynote Lecture: Airworthiness Requirements for<\/em>
\n Crashworthiness \u2013<\/em>
\nWim Doeland,
\nEASA<\/span><\/p>\n

8:40<\/strong> Overview of the Rotorcraft Crashworthiness Research<\/em>
\n Program at NASA Langley Research Center –<\/em>
\nKaren Jackson,
\nNASA, Langley Research Center<\/span><\/p>\n

9:00<\/strong> Development of a Fully Parameterized Process Chain to<\/em>
\n Evaluate the Crash Behavior of Transport Aircraft in the<\/em>
\n Preliminary Design Phase –<\/em>
\nD. Schwinn, D. Kohlgrueber, K. Harbig,
\nJ. Scherer –
\nGerman Aerospace Center (DLR), <\/span>
\nInstitute of Structures and Design<\/span><\/p>\n

9:20<\/strong> Crashworthiness Evaluation of a Metallic Narrow Body<\/em>
\n Transport Aircraft –<\/em>
\nGerardo Olivares, Vikas Yadav, Chandresh M. Zinzuwadia,
\nNational Institute for Aviation Research<\/span><\/p>\n

9:40<\/strong> Improvements in Aircraft Crashworthiness Impact<\/em>
\n Loads Modeling for Wheels-Up Landing Scenarios –<\/em>
\nAlan Melling, Luis H. Benitez Montanes, Hector Climent-
\nAirbus<\/span><\/p>\n

10:00<\/strong> Coffee and Tea Break<\/p>\n

10:20<\/strong> Prediction of Aircraft Structural Response during<\/em>
\n Ditching, an overview of the SMAES Project \u2013<\/em>
\nJ.C. Campbell –
\nSchool of Engineering, Cranfield University<\/span><\/p>\n

10:40<\/strong> Ditching Numerical Simulations: Recent Steps in Industrial<\/em>
\n Applications \u2013
\n<\/em>Luis Ben\u00edtez Monta\u00f1\u00e9s, H\u00e9ctor Climent M\u00e1\u00f1ez\u00a0\u2013
\nAirbus Military (EADS-CASA);<\/span>
\nMartin Siemann, Dieter Kohlgrueber \u2013
\nDeutsches Zentrum f\u00fcr Luft- und Raumfahrt (DLR)<\/span><\/p>\n

11:00<\/strong> Water Impact Tests and Simulations for CRM Scaled Aircraft Model \u2013<\/em>
\nHirokazu SHOJI \u2013 Aviation Program Group,
\nJapan Aerospace Exploration Agency;<\/span>
\nHiroyuki AKIYAMA \u2013
\nRyoyu Systems Co.,Ltd.;<\/span>
\nYoshiaki Hirakawa; Takehiko Takayama \u2013
\nYokohama National University;<\/span>
\nTsugikiyo Hirayama, Stuart C. McCallum, Masakatsu Minegishi, and Kazuo Iwasaki,
\nAviation Program Group, Japan Aerospace Exploration Agency<\/span><\/p>\n

11:20<\/strong> Crashworthiness Aspects of CFRP Airframe Sandwich<\/em>
\n Panels in Fold Core Design \u2013<\/em>
\nR. Sturm, Ch. Kindervater, H. Voggenreiter ,
\nGerman Aerospace Center (DLR), <\/span>
\nInstitute of Structures & Design<\/span><\/p>\n

11:40<\/strong> Characterization of Post-Failure Response of Riveted<\/em>
\n Junction for Crashworthy Applications –<\/em>
\nCACCHIONE B. \u2013
\nAWPARC: Agusta Westland Politecnico Advanced Rotorcraft Centre;<\/span>
\nAIROLDI A., ASTORI P. \u2013
\nPolitecnico di Milano<\/span><\/p>\n

12:00-1:00<\/strong> Lunch Break<\/p>\n

Technical Session 1B: Crashworthiness<\/span>
\n of Aircraft Interiors<\/span><\/h2>\n

1:00<\/strong> Keynote Lecture: Injury Criteria Development<\/em>
\n Methodology –<\/em>
\nJoseph Pellettiere,
\nFederal Aviation Administration<\/span><\/p>\n

1:20<\/strong> Kinematics of Lap Belt Restrained Occupants –<\/em>
\nRick Deweese,
\nFederal Aviation Administration\/Civil Aerospace<\/span>
\n Medical Institute<\/span><\/p>\n

1:40<\/strong> Modeling Standards Development Methodology –<\/em>
\nDavid Motorcraft,
\nFederal Aviation Administration\/Civil<\/span>
\n Aerospace Medical Institute<\/span><\/p>\n

2:00<\/strong> Certification by Analysis Methods for Aircraft Seat<\/em>
\n Structures per AC20-146 –<\/em>
\nGerardo Olivares, Nilesh Dohle \u2013
\nNational Institute for Aviation Research<\/span><\/p>\n

2:20<\/strong> Hybrid Certification: Merging Physical and Virtual
\nTesting-
\nTyler Smithson,
\nZodiac Aerospace<\/span><\/p>\n

2:40<\/strong> Computational Modeling Techniques for the Certification<\/em>
\n of an Innovative Aircraft Seat against Static Compliance<\/em>
\n (CS 25.561) –<\/em>
\nOmkar Gulavani, Rade Vignjevic, Kevin Hughes \u2013
\nCrashworthiness, Impact & Structural Mechanics Group, School<\/span>
\n of Engineering, Cranfield University<\/span><\/p>\n

3:00<\/strong> Coffee and Tea Break<\/p>\n

3:20<\/strong> Side-Facing Aircraft Seats Project Summary –<\/em>
\nRick Deweese,
\nFederal Aviation Administration\/Civil Aerospace<\/span>
\n Medical Institute<\/span><\/p>\n

3:40<\/strong> Human Body Model Evaluation for Aerospace Crashworthiness<\/em>
\n Applications –<\/em>
\nGerardo Olivares, Luis Gomez –
\nNational Institute for Aviation Research<\/span><\/p>\n

4:00<\/strong> Seat Cushion Replacement Project Update \u2013<\/em>
\nAmanda Taylor \u2013
\nFederal Aviation Administration\/Civil<\/span>
\n Aerospace Medical Institute<\/span><\/p>\n

4:20<\/strong> Using Airbag as a Pre-Acting Device to Improve Helicopter
\nCrew Seat Crashworthiness \u2013
\nZhiquing Chewng,
\nInfoScitex<\/span><\/p>\n

4:40<\/strong> Integrated Optimization of Helicopter Energy Absorbing<\/em>
\n Systems –<\/em>
\nPaolo Astori, Francesco Impari \u2013
\nPolitecnico di Milano<\/span><\/p>\n

5:00<\/strong> End Technical Session 1B<\/p>\n

Conference Dinner at the Kansas<\/span>
\n Cosmosphere and Space Center<\/span><\/h2>\n

5:15<\/strong> Bus Departure to Kansas Cosmosphere and Space
\nCenter in Hutchinson, KS<\/p>\n

6:15<\/strong> Arrival to Kansas Cosmosphere and Space Center
\nin Hutchinson, KS<\/p>\n

6:45<\/strong> Conference Dinner – Guest Speaker:
\nMatthew Melis,
\nNASA Glenn Research Center
\n\u201cContributions of Impact Testing<\/em>
\n and Analysis to the Space Shuttle Columbia Accident<\/em>
\n Investigation and Return to Flight\u201d<\/em><\/p>\n

8:30<\/strong> Bus Departure to Wichita<\/p>\n

<\/span><\/h5><\/div>\n

Day 2\u00a0– NOVEMBER 7th 2012
\n| NATIONAL CENTER FOR AVIATION TRAINING |<\/h2>\n

Technical Session 2A: High Velocity Impact<\/span><\/h2>\n

8:00<\/strong> Keynote Lecture: An Overview of Ballistic Impact Test<\/em>
\n Methods and Techniques in Aerospace Research and<\/em>
\n Development Applications –<\/em>
\nJ. Michael Pereira \u2013
\nNASA Glenn Research Center<\/span><\/p>\n

8:30<\/strong> Airworthiness Requirements for Impact Damage \u2013<\/em>
\nWim Doeland,
\nEASA<\/span><\/p>\n

8:50<\/strong> Damage Criticality and Inspection Concerns of<\/em>
\n Composite \u2013 Metallic Aircraft Structures Subjected to High<\/em>
\n Energy, Low Velocity Blunt Impact-<\/em>
\nPeter Bishop \u2013
\nBishop GmbH<\/span><\/p>\n

9:10<\/strong> Development and Validation of a Gelatin Bird Substitute-<\/em>
\nGerardo Olivares, Maria Tufano, Nilesh Dohle \u2013
\nNational Institute for Aviation Research;<\/span>
\nJ. Michael Pereira, Duane M. Revilock, \u2013
\nNASA Glenn Research Center<\/span><\/p>\n

9:30<\/strong> Fundamental Research of Bird-Strike Simulation –<\/em>
\nStuart McCallum, Hirokazu SHOJI \u2013
\nAviation Program Group,<\/span>
\n Japan Aerospace Exploration Agency \u2013<\/span>
\nHiroyuki AKIYAMA \u2013
\nRyoyu Systems Co., Ltd.<\/span><\/p>\n

9:50<\/strong> Helicopter Bird-Strike \u2013 Accident Investigation and Safety<\/em>
\n Recommendations \u2013<\/em>
\nCarl R. Schultheisz, Ph.D. \u2013
\nNational Transportation Safety Board<\/span><\/p>\n

10:10<\/strong> Design Criteria for Birdstrike Damage on Windshield –<\/em>
\nA. Grimaldi , A. Sollo \u2013 Piaggio Aero Industries; F. Marulo, M. Guida \u2013
\nUniversit\u00e0 di Napoli \u201cFederico II”<\/span><\/p>\n

10:30<\/strong> Coffee Break<\/p>\n

10:40<\/strong> Use of \u201cRealistic Simulation\u201d (Abaqus\/Explicit) for Bird<\/em>
\n Impact Sizing and Certification of A400M Leading Edges –<\/em>
\nEtienne Maillard \u2013
\nSONACA S.A.<\/span><\/p>\n

11:00<\/strong> Application of Smooth Particle Hydrodynamics (SPH)<\/em>
\n Technique to Modeling Bird-Strike on Composites –<\/em>
\nMahesh Turaga, Kyle Indermuehle, Vladimir S. Sokolinsky \u2013
\nDS Simulia<\/span><\/p>\n

11:20<\/strong> Methodology and Experience for Launching Birds, ice<\/em>
\n and Many Different Foreign Objects to High Velocity and<\/em>
\n Monitoring Target Response –<\/em>
\nScott Mullin, Donald Grosch, James Mathis, Rory Bigger \u2013
\nEngineering Dynamics Department,<\/span>
\n Southwest Research Institute<\/span><\/p>\n

11:40<\/strong> Influence of Pre-load on the Impact Behavior of Panels:<\/em>
\n Damage Tolerance Aspects –<\/em>
\nN. Toso-Pentec\u00f4te*, A.F. Johnson \u2013
\nGerman Aerospace Center (DLR) <\/span>
\nInstitute of Structures and Design<\/span><\/p>\n

12:00-1:00<\/strong> Lunch Break<\/p>\n

<\/span><\/h5><\/div>\n

Technical Session 2B: Dynamic Behavior<\/span>
\n Material Characterization<\/span><\/h2>\n

1:00<\/strong> Testing Composites at High Rates: Results, Simulations and<\/em>
\n Challenges –<\/em>
\nSidney Chocron, Charles E. Anderson, Scott Mullin\u2013
\nSouthwest Research Institute (SWRI)<\/span><\/p>\n

1:20<\/strong> Coupon Level High Strain Round Robin Testing Program \u2013<\/em>
\nJuan Felipe Acosta, Gerardo Olivares ,
\nNational Institute for Aviation Research;<\/span>
\nSuresh Keshavanarayana, Dept. Aerospace Engineering.,
\nWichita State University;<\/span>
\nAllan Abramowitz –
\nFAA;<\/span>
\nB. Mobasher –
\nArizona State University;<\/span>
\nA. Johnson, M. David \u2013
\nDLR;<\/span>
\nA. Gilat
\nOhio State University;<\/span>
\nY. Wang, D. Erdman III, M. Starbuck –
\nOakridge National Labs<\/span><\/p>\n

1:40<\/strong> Effect of Strain Rate on the Failure Mechanisms and<\/em>
\n Energy Absorption in Polymer Composite Elements under Axial<\/em>
\n Loading \u2013<\/em>
\nM. David, A. F. Johnson and H. Voggenreiter-
\nGerman Aerospace Center (DLR), <\/span>
\nInstitute of Structures and Design<\/span><\/p>\n

2:00<\/strong> Impact Characterization of a Multifunctional Composite<\/em>
\n Panel –<\/em>
\nTeo Mudric, Alessandro Francesconi, Ugo Galvanetto,
\nCinzia Giacomuzzo, Mirco Zaccariotto \u2013 CISAS \u2013 \u201cG. Colombo\u201d
\nCenter of Studies and Activities for Space, <\/span>
\nUniversity of Padova<\/span><\/p>\n

2:20<\/strong> Load Signal Modulation During Dynamic Tension Tests –<\/em>
\nSuresh Keshavanarayana, Dept. Aerospace Engineering.,
\nWichita State University;<\/span>
\nG. Olivares and J.F. Acosta,
\nNational Institute for Aviation Research<\/span><\/p>\n

2:40<\/strong> Stroke Rates and Strain Rates: A Parametric Study –<\/em>
\nSuresh Keshavanarayana \u2013 Dept. Aerospace Engineering,
\nWichita State University<\/span><\/p>\n

3:00<\/strong> Three Point Bending Hopkinson Bar for Fracture<\/em>
\n Toughness Measurement: A New Approach for Data Processing-<\/em>
\nJ. Mart\u00ednez-Figueroa, C. Rubio-Gonzalez, F. Velasco-Reyes \u2013
\nCentro de Ingenier\u00eda y Desarrollo Industrial;<\/span>
\nN. Benseddiq \u2013
\nLaboratoire de M\u00e9canique de Lille IUT-A GMP, Universit\u00e9 de Lille<\/span><\/p>\n

3:20<\/strong> Effects of Structural Geometry on Crashworthiness of<\/em>
\n Carbon\/Epoxy Composites –<\/em>
\nJames M. Hobbs, Marc A. Courteau,
\nand Daniel O. Adams \u2013
\nDepartment of Mechanical Engineering,<\/span>
\n University of Utah;<\/span>
\nRichard Roberts and Graham Barnes \u2013
\nEngenuity Limited<\/span><\/p>\n

3:40<\/strong> Predicting Crashworthiness of Composite Laminates Using<\/em>
\n Ply Decomposition –<\/em>
\nTimothy Francis, James Hobbs, and Daniel O. Adams \u2013
\nDepartment of Mechanical Engineering, <\/span>
\nUniversity of Utah;<\/span>
\nRichard Roberts and Graham Barnes \u2013
\nEngenuity Limited<\/span><\/p>\n

4:00<\/strong> Postbifurcation Shear Stability of Composite Wing Spars<\/em>
\n using Nonlinear Modelling and Continuum Damage Mechanics-<\/em>
\nJavier Herrero,
\nThe Boeing Company<\/span><\/p>\n

4:20<\/strong> An Easy and Accurate Method for Fitting Material Strength<\/em>
\n Model Parameters from Quasi static and Split Hopkinson Bar<\/em>
\n Tensile Tests –<\/em>
\nJonathan P. Glanville \u2013
\nANSYS, Inc<\/span><\/p>\n

4:40<\/strong> Composite Materials Characterization Methods for More
\nReliable Simulation of Blade Containment in Jet Engines \u2013
\nRobert K. Goldberg, Gary D. Roberts, Lee W. Kohlman and J. Michael
\nPereira –
\nNASA Glenn Research Center,<\/span>
\nChristopher R. Cater-
\nMichigan State University<\/span><\/p>\n

5:00<\/strong> Closing Remarks, Workshop Summary,
\nAnnouncement of 2014 Location – Gerardo Olivares , NIAR<\/p>\n","protected":false},"excerpt":{"rendered":"

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