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AE 451
Aeroelasticity
Credit: 3 or 4 hours.
(A A E 351) Advanced fundamental treatment of aerodynamic and dynamic structural phenomena associated with flexible airplanes and missiles; divergence of linear and nonlinear elastic lifting surfaces; effect of elastic and inelastic deformations on lift distributions and stability; elastic flutter of straight and swept wings; equations of disturbed motion of elastic and inelastic aircraft; dynamic response to forces, gusts, and continuous atmospheric turbulence; creep divergence of lifting surfaces; flutter in the presence of creep; and effect of temperature on inelastic divergence and flutter. 3 undergraduate hours. 3 or 4 graduate hours. Prerequisite: AE 352 or TAM 412; AE 322 or TAM 251.
Section Information
| CRN | Type | Section | Time | Days | Location | Instructor |
| 39823 | lecture- discussion | A3 | 08:30 AM - 09:50 AM | TR | room 225A
Talbot Laboratory | Bergman, L |
3 hours
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| 39824 | lecture- discussion | A4 | 08:30 AM - 09:50 AM | TR | room 225A
Talbot Laboratory | Bergman, L |
4 hours
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