Page 52 - ASME IMECE 2015 Program

Technical Program TRACK 1

TRACK 1 Advances in Aerospace Technology 2:09pm
Robust Optimal Trailing-Edge Flaps for Helicopter Vibration Reduction for
Various Flying Conditions
MONDAY, NOVEMBER 16 Technical Paper Publication. IMECE2015-53150

Saijal Kizhakke Kodakkattu, Government Engineering College Kozhikode,
1-1 Calicut, India, Prabhakaran Nair, M.L. Joy, National Institute of Technology
PLENARY Calicut, Calicut, India
2:27pm
1-1-1 Aeroelasticity of Highly Flexible Morphing Aircraft with Wing Camber De-
PLENARY SESSION I formations
Technical Presentation. IMECE2015-52846

360A 10:30am–12:00pm Nathan Butler, Cecilia King, Weihua Su, University of Alabama, Tuscaloosa,
AL, United States
Session Chair: Olesya Zhupanska, University of Iowa, Iowa City, IA, United
States
10:30am 1-8
Beyond Buckling: A Challenge for Aircraft Composite Structures IMPACT, DAMAGE, AND FRACTURE OF COMPOSITE STRUCTURES
Plenary Presentation. IMECE2015-54192

Chiara Bisagni, TU Delft, Delft, Netherlands 1-8-1
IMPACT, DAMAGE, AND FAILURE OF COMPOSITES I

1-4 360B 1:15pm–2:45pm
AEROMECHANICS AND AEROELASTICITY
Session Chair: Kwek Tze Tan, University of Akron, Akron, OH, United States
Session Co-Chair: Ali Najafi, ANSYS Inc., Houston, TX, United States
1-4-1
AEROMECHANICS AND AEROELASTICITY 1:15pm
Characterization of Resin-Injection Repair of Impact Damage in Polymer
Matrix Composite
360A 1:15pm–2:45pm Technical Paper Publication. IMECE2015-50400

Session Chair: Weihua Su, University of Alabama, Tuscaloosa, AL, United Ritwik Moghe, Raghu Prakash, Deepika Sudevan, Indian Institute of Tech-
States nology Madras, Chennai, Tamilnadu, India, Hema Katta Shambhayya, Aero-
Session Co-Chair: Zahra Sotoudeh, Rensselaer Polytechnic Institute, Troy, nautical Development Establishment, Bangalore, Karnataka, India
NY, United States
1:33pm
1:15pm Strain Rate Dependent Failure of Glass/Epoxy Interfaces and Correspond-
Accelerating RBF-Based Mesh Deformation by Implementing an Agglom- ing Composite Structures via Nanoimpact Experiments
eration Strategy Technical Presentation. IMECE2015-51099
Technical Paper Publication. IMECE2015-50902
Devendra Verma, Vikas Tomar, Purdue University, West Lafayette, IN, Unit-
Giorgos Strofylas, Georgios Lygidakis, Ioannis Nikolos, Technical Universi- ed States
ty of Crete, Chania, Greece
1:51pm
1:33pm Identification of Location and Magnitude of Impact Force on a Composite
Airfoil Optimization Using Area-Preserving Free-Form Deformation Sandwich Structure with Lattice Truss Core
Technical Paper Publication. IMECE2015-50904 Technical Paper Publication. IMECE2015-51411

Stavros Leloudas, Giorgos Strofylas, Ioannis Nikolos, Technical University Hamed Kalhori, Lin Ye, University of Sydney, Sydney, NSW, Australia, Zheng
of Crete, Chania, Greece Li, Bing Li, Peking University, Beijing, China
1:51pm 2:09pm
Finite Element Analysis, Ground Vibration Testing, and Characterization Damage Simulation of Stitched CFRP Laminates under High-Velocity Pro-
of Vibration Modes for a Cantilever Plate Representing an Aircraft Wing jectile Impact
with and without Secondary Structure Attached Technical Paper Publication. IMECE2015-52467
Technical Paper Publication. IMECE2015-51020
Akinori Yoshimura, Japan Aerospace Exploration Agency, Mitaka, Tokyo,
Santosh Nedukanjirathingal, Spirit AeroSystems Inc., Wichita, KS, United Japan, Yasuhito Mikami, Tokyo Metropolitan University, Hino, Tokyo, Japan,
States, Yi Yang Tay, Wichita State University, Farmington, MI, United States, Masahiro Nakayama, Toshio Ogasawara, Japan Aerospace Exploration
Hamid Lankarani, Wichita State University, Wichita, KS, United States Agency, Mitaka, Tokyo, Japan, Naoyuki Watanabe, Tokyo Metropolitan Uni-
versity, Hino, Tokyo, Japan
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