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ASIDIC 2019 : Aerospace Structural Impact Dynamics International Conference

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Link: http://asidiconference.org/
 
When Jun 4, 2019 - Jun 6, 2019
Where Madrid, Spain
Submission Deadline Sep 15, 2018
Notification Due Oct 5, 2018
Final Version Due May 5, 2019
Categories    aerospace   impact   structural   UAV
 

Call For Papers

The fourth edition of the Aerospace Structural Impact Dynamics International Conference is being held June 4th-6th 2019, at the University Carlos III de Madrid (UC3M) in Madrid, Spain. The conference will once more provide a forum for researchers, regulatory agencies and industry professionals to present and discuss the latest aerospace crashworthiness regulations, structural impact dynamics, computational & experimental techniques, technologies and current research.

The 2019 edition of the ASIDI Conference will be comprised of four technical sessions, two technical workshops, two keynote speaker presentations, and two keynote lectures.

All abstracts submitted for the 2019 edition of the ASIDI Conference must meet the following requirements in order to be considered:

• Criteria for evaluation: All papers will be considered, but you must submit an EXTENDED ABSTRACT consisting of 500-1,000 words, along with the author’s name(s), company/institution, short author bio, and contact details.

• The submission must include sufficient detail to demonstrate to the conference scientific committee the purpose of the paper, the technical foundation for the topics to be discussed, any preliminary results to date, and the expected results of the final paper, including key figures, and references, as appropriate.

THE CONFERENCE PROGRAM WILL COVER THE FOLLOWING TOPICS:
I. Aerospace Crashworthiness

Crashworthiness of Composites and Metallic Aerospace Structures:

i. Structural Design

ii. Experimental and Computational Methods

iii. Ditching/Soil Impact

iv. Accident Reconstruction

Crashworthiness of Aircraft Interiors:

i. Aerospace vATD Developments

ii. Advanced Restraint Systems

iii. Aerospace Seat Modeling Techniques: Computational and Experimental methods

iv. Certification by Analysis Methodology: Seat Structures

v. Seat Design with Composites and Advanced Materials

II. High and Low Velocity Impact

Bird Strike Analysis

Hail Impact

Foreign Object Damage

Low Velocity Impact Damage

UAS Crashworthiness

III. Composite and Metallic Materials-Dynamic Behavior Material Characterization

Experimental and Computational Methods

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