๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Aeroelastic response and stability analysis of composite rotor blades in forward flight

โœ Scribed by S.M. Jeon; I. Lee

Publisher
Elsevier Science
Year
2001
Tongue
English
Weight
190 KB
Volume
32
Category
Article
ISSN
1359-8368

No coin nor oath required. For personal study only.

๐Ÿ“œ SIMILAR VOLUMES

Aeroelastic analysis of composite rotor
Aeroelastic analysis of composite rotor blades in hover
โœ Seong Min Jeon; Maeng Hyo Cho; In Lee ๐Ÿ“‚ Article ๐Ÿ“… 1998 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 776 KB

The aeroelastic phenomena of a composite rotor blade in hover is investigated using a finite element method. A large deflection type beam theory is used for the one-dimensional global deformation analysis of the hingeless, isolated rotor undergoing arbitrary large displacements and rotations, but sm

Almost-sure asymptotic stability of roto
Almost-sure asymptotic stability of rotor blades flapping motion in forward flight in turbulent flow
โœ N. Sri Namachchivaya; J.E. Prussing ๐Ÿ“‚ Article ๐Ÿ“… 1991 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 641 KB

This paper examines the almost-sure asymptotic stability of uncoupled flapping motion of rotor blades in forward flight under the effect of atmospheric turbulence. Under these conditions, the equation of motion of the rotor blade system contains both harmonic and stochastic excitations. The intensit

Design and aeroelastic analysis of activ
Design and aeroelastic analysis of active twist rotor blades incorporating single crystal macro fiber composite actuators
โœ Jae-Sang Park; Ji-Hwan Kim ๐Ÿ“‚ Article ๐Ÿ“… 2008 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 442 KB

The advanced active twist rotor (AATR) blade incorporating single crystal macro fiber composite (single crystal MFC) actuators is designed and the aeroelastic analysis is performed. The AATR blade is designed based on an existing passive blade and the NASA/ ARMY/MIT active twist rotor (ATR) prototyp