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Monday, 9:30 AM - 12:00 PM

Technical

Presentations

Note: Presentations may start a few minutes before the time listed in the schedule.

Participant RoleDetailsStart TimeMinutesAction
SubmissionFinite Element Modeling of an Origami-Inspired Deployable Solar Panel for Cubesat Applications09:30 AM30View
SubmissionAre There Cases in Which Classical Beam Theories Fail to Compute the Fundamental Frequency?10:00 AM30View
SubmissionDynamic Analysis of Variable Thickness Shells in Aerospace Applications via Cuf Adaptive Finite Elements10:30 AM30View
SubmissionSlope-Inertia Model for Rotating Timoshenko-Ehrenfest Beams11:00 AM30View
SubmissionVibration Reduction of a Lift-Offset Co-Axial Rotorcraft System Using Individual Blade Control Approach11:30 AM30View
Total:150 Minute(s)

02-01-01: Dynamic Loads, Response, Vibration and Alleviation of Aerospace Structures - I