It is well known that the presence of non-linearities may signi"cantly a!ect the aeroelastic response of an aerospace vehicle structure. In this paper, the aeroelastic behaviour at high Mach numbers of an all-moving control surface with a non-linearity in the root support is investigated. Very often
✦ LIBER ✦
“In-the-large” behaviour of an inverted pendulum with linear stabilization
✍ Scribed by M.G. Henders; A.C. Soudack
- Publisher
- Elsevier Science
- Year
- 1992
- Tongue
- English
- Weight
- 866 KB
- Volume
- 27
- Category
- Article
- ISSN
- 0020-7462
No coin nor oath required. For personal study only.
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