AER 722
Aeroelasticity
Wing divergence. Control surface effectiveness. Flexibility effects on aircraft stability and control. Quasi-Steady and unsteady aerodynamics. Flutter analysis of two-dimensional wings with discussion of three-dimensional effects. Introduction of other aeroelastic phenomena such as stall flutter and buffeting. Prevention of aeroelastic instabilities. Flight flutter testing.
Weekly Contact: Lecture:3 hrs.
GPA Weight: 1.00
Course Count: 1.00
Billing Units: 1
Antirequisites
None
Co-Requisites
None
Custom Requisites
None
Mentioned in the Following Calendar Pages
*List may not include courses that are on a common table shared between programs.
- AER 814 - Aircraft Design Project
- Aerospace Engineering
-
AER 222
Engineering Design and Graphical Communication -
AER 309
Basic Thermodynamics -
AER 316
Fluid Mechanics -
AER 318
Dynamics -
AER 320
Statics and Intro to Strength of Materials -
AER 403
Mechanisms and Vibrations -
AER 404
Intro to Aerospace Engineering Design -
AER 416
Flight Mechanics -
AER 423
Thermodynamics and Heat Transfer -
AER 504
Aerodynamics -
AER 507
Materials and Manufacturing -
AER 509
Control Systems -
AER 520
Stress Analysis -
AER 606
Component Design and Material Selection -
AER 615
Aircraft Performance -
AER 621
Aerospace Structural Design -
AER 622
Gas Dynamics -
AER 626
Applied Finite Elements -
AER 627
Introduction to Space Robotics -
AER 710
Propulsion -
AER 715
Avionics and Systems -
AER 716
Aircraft Stability and Control -
AER 721
Orbital Dynamics -
AER 722
Aeroelasticity -
AER 723
Introduction to Space Systems Design -
AER 813
Space Systems Design Project -
AER 814
Aircraft Design Project -
AER 817
Systems Engineering -
AER 818
Manufacturing Management -
AER 821
Spacecraft Attitude Dynamics and Control -
AER 822
Avionics Design Project -
AER 827
Composite Materials -
AER 870
Aerospace Engineering Thesis