(1) "Policy and Oversight: Technical Corrosion Collaboration"

Scott Fawaz

Office of Undersecretary of Defense, USA

Acquisition Technology and Logistics

Summary: DoD Response to Corrosion Issues: National Defense Authorization Act, Military Equipment and Infrastructure, Prevention and Mitigation of Corrosion.

 

(2) "AIRWORTHINESS & NEW DEVELOPMENTS IN AIRCRAFT STRUCTURES"

Demetrios Papacostas

CEO at Hellenic Aerospace Industry, Greece

Senior Executive, Corporate Officer and Board Chairman

Summary: In Hellenic Aerospace Ind. new methods are developed for sensorized structures, preparing the technology background and demonstrators, for the manufacturing of the next generation European Aircraft and contributing in the supply chain of the major European OEMs. An overview is presented for the specific technologies and research activities. Novel smart health monitoring systems embedded in critical aircraft components and networks are incorporated with different sensors to enhabce reliability, efficiency, damage detection capability and economic benefit.

 

(3) "Fatigue Life Prediction and Surface Enhnancement of Aeronautical Materials in China"

Zheng Zhong*

Dean of School of Aerospace Engineering and Applied Mechanics,Tongji University, Shanghai 200092, China

Yukui Ga

Professor of School of Aerospace Engineering and Applied Mechanics, Tongji University, Shanghai 2000092, China

Summary: Fatigue properties of high strength metallic materials for aircrafts are summarized and a fatigue life prediction method based on small crack theory is proposed. Recent developments of surface enhancements such as laser peening, shot peening, cold hole expansion are employed to increase the fatigue performance of high strength aeronautical  metals. Evaluation of the effects of residual stresses on fatigue life of materials is discussed.

* Presenting author


(4) "Research related to fatigue durability and structural health monitoring for aircrafts in Russia"

Sergey Panin*

Deputy Director of Inst. of Strength Phys. & Mat. Sci., Tomsk

Victor Panin

Adviser of Russian Academy of Sciences, Head of Laboratory, Inst. of Strength Phys. & Mat. Sci., Tomsk

Victor Sergeev

Deputy Director of Inst. of Strength Phys. & Mat. Sci., Tomsk

Mikhail Burkov

Researcher of Inst. of Strength Phys. & Mat. Sci.,Tomsk

Pavel Luybutin

Researcher of Inst. of Strength Phys. & Mat. Sci.,Tomsk

Summary: Recent developments of material science are related to the modification of structure and properties of traditionally used alloys. Higher fatigue durability can be obtained by precision treatment of surface. High-temperature ceramic coating can improve the operating temperatures. Smart coatings can further sustain severe operating conditions. Life prediction methods are developed for fatigue and fracture of structural materials to enhance operation safety and more effective use of the structural health monitoring system.

* Presenting author

 

(5) "Fatigue of Polymer Composites: Characterization, Analysis and Interpretation of Fatigue Crack Growth"

Steffen Stelzer*

Institute for Materials Science and Testing of Plastics, Montanuniversity Leoben, Leoben, Austria

Andreas J. Brunner

Laboratory for Mechanical Systems Engineering, Empa, Swiss Federal Laboratories for Materials Science and Technology, Duebendorf, Switzerland

Rhys Jones

Centre of Expertise in Structural Mechanics, Department of Mechanical & Aerospace Engineering, Monash University, Clayton, Australia

Summary: Recent experimental characterization of cyclic fatigue crack growth in carbon-fiber polymer composite specimens has high-lighted a number of issues that have potential relevance for the "no-growth" design philosophy for composite structures and for fatigue life prediction.

* Presenting author

 

(6) ''Innovative Life Prediction Technology of Aero Engines"

Tu Shan-Tung

United Innovation Center (UIC) of Life Prediction Technology of Aero Engines,

East China University of Science and Technology (ECUST)

Summary: The Aviation Industry Corp of China (AVIC) has planned to Invest billions of USD for aero engine research and development. The UIC shall be involved as a part of this effort. The lecture will provide some comparisons of current life prediction methods and new techniques for life design of future engines.

 

(7) ''Linear and Nonlinear Lamb Wave SHM for Composite Materials and Structures''

Dimitris Saravanos

Dept. of Mechanical Engineering & Aeronautics, University of Patras, Greece

Summary: In this presentation we will first review research work on active SHM methods based on the linear wave propagation of Lamb waves.  Numerical results from semi-analytical solutions and FEA models will illustrate the propagation of guided waves in laminated composite strips. Experimental results will further demonstrate the capability of ultrasonic Lamb waves to detect small delamination cracks, matrix cracks and impact damage in composite strips.