The Effects of Damage and Uncertainty on the Aeroelastic /Aeroservoelastic Behavior and Safety of Composite Aircraft
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1 AMTAS Autumn Meeting March 16, 2010 The Effects of Damage and Uncertainty on the Aeroelastic /Aeroservoelastic Behavior and Safety of Composite Aircraft Presented by Francesca Paltera UW Mechanical Engineering
2 Outline Motivation Objectives Background Review Past Accomplishments Recent Progress Future Work AMTAS Impact
3 Motivation Understand effects of uncertainty on composite Aeroservoelastic structures in terms of Flutter and Limit Cycle Oscillations (LCO) Obtain experimental benchmark results for industry Develop automated computational tools for simulation of uncertain aeroelastic structures Establish collaborative expertise
4 Objectives Build an experimental model and carry out aeroelastic/ wind tunnel tests to Flutter and Limit Cycle Oscillations (LCO) Implement Uncertainty: local nonlinearities (damage, free play, broken actuator) and global nonlinearities (broken hinge) Develop automated computational tools for simulation of Flutter and LCO in presence of nonlinearities
5 Background
6 Background
7 Background
8 Background
9 Review Past Accomplishments Wing Design Control Surface (aileron, flap, rudder) Airfoil
10 Review Past Accomplishments Wing Design
11 Review Past Accomplishments Wing Design UGS Unigraphics
12 Review Past Accomplishments Wing Design Hinge Tube Carbon Fiber Skin Foam Core Hinge Slots 1
13 Review Past Accomplishments Wing Design
14 Review Past Accomplishments Wing Manufacturing
15 Review Past Accomplishments Wing Manufacturing
16 Review Past Accomplishments Induced Damage
17 Review Past Accomplishments Wind Tunnel Fixture
18 Review Past Accomplishments Wind Tunnel Fixture
19 Review Past Accomplishments Analytical Development for pristine structure
20 Review Past Accomplishments Flutter Tests
21 Review Past Accomplishments Flutter Tests Flutter speed was decreased: As the distance between the cg of the control surface and the hinge line was increased Due to delamination between skin and core Due to induced free-play (localized hinge bearing damage) Due to free-rotation (broken actuator)
22 Recent Progress Freeplay
23 Recent Progress Improved Control Surface Design
24 Recent Progress Improved Control Surface Design
25 Recent Progress Improved Control Surface Design
26 Recent Progress Improved Control Surface Design
27 Recent Progress Non Linear Damper
28 Recent Progress Non Linear Damper
29 Recent Progress Non Linear Damper
30 Recent Progress Non Linear Damper
31 Future Work Customize damper response through design (HELP!) Non-linear damper characterization Continue wind tunnel experiments on the wing model WITH non-linearities Develop automated computational tools for dynamic behavior simulation of non-linear aeroelastic models
32 AMTAS Impact Networking with Industry and Government Experts Developing Mentors Technical Talks Converging onto a Carrier Path
33 Contributors Thank you! Department of Mechanical Engineering Francesca Paltera, PhD student Dr. Mark Tuttle, co-pi, professor and chairman Department of Aeronautics and Astronautics Dr. Eli Livne PI, Professor Boeing Commercial, Seattle Dr. James Gordon, Associate Technical Fellow, Flutter Methods Development Dr. Kumar Bhatia, Senior Technical Fellow, Aeroelasticity and Multidisciplinary Optimization Curing FAA Technical Monitor Curtis Davies, Program Manager of JAMS, FAA/Materials & Structures Future Work Other FAA Personnel Involved Dr. Larry Ilcewicz, Chief Scientific and Technical Advisor for Advanced Composite Materials Carl Niedermeyer, Airframe and Cabin Safety Branch (ANM-115), Standards Staff - Transport Airplane Directorate (previously: Boeing flutter manager for the 787 and 747 programs)
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