Basic Information
Static Aeroelasticity# Strip Theory, Divergence, Control Surface Effectiveness and Reversal, Wing Sweep Effects. Structural Modal Approach. Unsteady Aeroelasticity# Unsteady Aerodynamics, Wing And Control Surface Flutter, Gust Response. Learning Outomes# On Completions of The Course The Student Will Be Able To# 1. Familiarization With The Scope of Aeroelasticity and With Basic Terms and Topics of Static Aeroelasticity. 2. Ability to Develop And Use Computational Tools For Static Aeroelastic Analysis. 3. Deepen The Knowledfge of Static Aeroelastic Phenomena. 4. Understand Control Surface Effectiveness. 5. Ability to Develop and Use Computational Tools For Modal Analysis. 6. Familiarization With Unsteady Aerodynamics and Analytical Tools For Unsteady Aerodynamics. 7. Understand Flutter. 8. Ability to Develop and Use Computational Tools For Flutter Analysis. 9. Deepen The Knowledge of Various Flutter Analysis Tools and Mechanisms. 10. Familiarization With Advanced Non- Linear Unsteady Aeroelasticity Problems. 11. Familiarization With Gust Response. 11. Ability to Develop and Use Compputational Tools For Gust Response. 12. Familiarization With Advanced Non-linear Gust Response Problems.
Faculty: Aerospace Engineering
|Graduate Studies
Pre-required courses
(84225 - Dynamics and 84312 - כונסים ונחירים and 84515 - Introduction to Theory of Elasticity) or (84312 - כונסים ונחירים and 84515 - Introduction to Theory of Elasticity and 114101 - Analytical Mechanics)
Semestrial Information
Weekly Hours
3 Academic Credit • 3 Lecture Hours
Responsible(s)
Ariel Drachinsky
Registration Groups
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Weekly Hours
3 Academic Credit • 3 Lecture Hours
Responsible(s)
Daniella Raveh
Registration Groups
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Weekly Hours
3 Academic Credit • 3 Lecture Hours
Responsible(s)
Daniella Raveh
Registration Groups
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