๐”– Bobbio Scriptorium
โœฆ   LIBER   โœฆ

Flutter analysis for control surface of launch vehicle with dynamic stiffness

โœ Scribed by Seung-Kil Paek; In Lee


Publisher
Elsevier Science
Year
1996
Tongue
English
Weight
619 KB
Volume
60
Category
Article
ISSN
0045-7949

No coin nor oath required. For personal study only.


๐Ÿ“œ SIMILAR VOLUMES


Design of controller switching strategy
โœ Hayato Komatsu; Tatsuya Suzuki; Shigeru Okuma ๐Ÿ“‚ Article ๐Ÿ“… 2008 ๐Ÿ› John Wiley and Sons ๐ŸŒ English โš– 583 KB

## Abstract When a reusable launch vehicle (RLV) returns to earth, it flies just by gliding without thrust. In this phase, one of the most likely and important faults to occur in the airframe is a jamming of the elevon. To tolerate this failure, the flight control system must keep stability and per

ON THE DYNAMICS OF FLIGHT VEHICLE CONTRO
โœ Shih-Ming Yang; S.H. Chao ๐Ÿ“‚ Article ๐Ÿ“… 1996 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 375 KB

The influence of structure modal parameters on the dynamics of an integrated actuator and control surface system is studied in this paper. The control surface is modeled as a uniform thickness plate mounted on a push-pull hydraulic actuator. The transfer function between the command and measurement

DYNAMIC STIFFNESS ANALYSIS FOR IN-PLANE
โœ Y.-P. Tseng; C.S. Huang; C.-J. Lin ๐Ÿ“‚ Article ๐Ÿ“… 1997 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 232 KB

This paper provides a systematic approach to solve in-plane free vibrations of arches with variable curvature. The proposed approach basically introduces the concept of dynamic stiffness matrix into a series solution for in-plane vibrations of arches with variable curvature. An arch is decomposed in

DYNAMIC STIFFNESS ANALYSIS FOR TORSIONAL
โœ Y. MATSUI; T. HAYASHIKAWA ๐Ÿ“‚ Article ๐Ÿ“… 2001 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 279 KB

An analytical method for determining natural frequencies and mode shapes of the torsional vibration of continuous beams with thin-walled cross-section is developed by using a general solution of the di!erential equation of motion based on Vlasov's beam theory. This method takes into account the e!ec