𝔖 Bobbio Scriptorium
✦   LIBER   ✦

NEAR-WAKE FLOW STRUCTURE OF A CYLINDER WITH A HELICAL SURFACE PERTURBATION

✍ Scribed by C.-K. CHYU; D. ROCKWELL


Publisher
Elsevier Science
Year
2002
Tongue
English
Weight
597 KB
Volume
16
Category
Article
ISSN
0889-9746

No coin nor oath required. For personal study only.


πŸ“œ SIMILAR VOLUMES


AN INVESTIGATION OF STABILITY IN THE LAR
✍ A.P. LEWIS πŸ“‚ Article πŸ“… 2002 πŸ› Elsevier Science 🌐 English βš– 475 KB

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