Smart Helicopter Rotors (Record no. 80735)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 04741nam a22006495i 4500 |
| 001 - CONTROL NUMBER | |
| control field | 978-3-319-24768-7 |
| 005 - DATE AND TIME OF LATEST TRANSACTION | |
| control field | 20220801222416.0 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 151215s2016 sz | s |||| 0|eng d |
| 020 ## - INTERNATIONAL STANDARD BOOK NUMBER | |
| ISBN | 9783319247687 |
| -- | 978-3-319-24768-7 |
| 082 04 - CLASSIFICATION NUMBER | |
| Call Number | 629.1 |
| 100 1# - AUTHOR NAME | |
| Author | Ganguli, Ranjan. |
| 245 10 - TITLE STATEMENT | |
| Title | Smart Helicopter Rotors |
| Sub Title | Optimization and Piezoelectric Vibration Control / |
| 250 ## - EDITION STATEMENT | |
| Edition statement | 1st ed. 2016. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Number of Pages | XIII, 257 p. 213 illus. |
| 490 1# - SERIES STATEMENT | |
| Series statement | Advances in Industrial Control, |
| 505 0# - FORMATTED CONTENTS NOTE | |
| Remark 2 | Introduction -- Mathematical Modeling -- Preliminary Studies with Active Flaps -- Flap Configuration and Control Law -- Active Flap Controller Evaluation -- Trailing-edge Flap Placement -- Piezoceramic Actuator Hysteresis -- Active Rotating Beams -- Box-beam Active Rotor Blade -- Airfoil-section Rotor Blade -- Dynamic Stall Alleviation Using Active Twist -- Appendices: Kinetic- and Strain-Energy Terms; Section Properties; Shape Functions for Space; Shape Functions for Time. |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | Exploiting the properties of piezoelectric materials to minimize vibration in rotor-blade actuators, this book demonstrates the potential of smart helicopter rotors to achieve the smoothness of ride associated with jet-engined, fixed-wing aircraft. Vibration control is effected using the concepts of trailing-edge flaps and active-twist. The authors’ optimization-based approach shows the advantage of multiple trailing-edge flaps and algorithms for full-authority control of dual trailing-edge-flap actuators are presented. Hysteresis nonlinearity in piezoelectric stack actuators is highlighted and compensated by use of another algorithm. The idea of response surfaces provides for optimal placement of trailing-edge flaps. The concept of active twist involves the employment of piezoelectrically induced shear actuation in rotating beams. Shear is then demonstrated for a thin-walled aerofoil-section rotor blade under feedback-control vibration minimization. Active twist is shown to be significant in reducing vibration caused by dynamic stall. The exposition of ideas, materials and algorithms in this monograph is supported by extensive reporting of results from numerical simulations of smart helicopter rotors. This monograph will be a valuable source of reference for researchers and engineers with backgrounds in aerospace, mechanical and electrical engineering interested in smart materials and vibration control. Advances in Industrial Control aims to report and encourage the transfer of technology in control engineering. The rapid development of control technology has an impact on all areas of the control discipline. The series offers an opportunity for researchers to present an extended exposition of new work in all aspects of industrial control. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Thakkar, Dipali. |
| 700 1# - AUTHOR 2 | |
| Author 2 | Viswamurthy, Sathyamangalam Ramanarayanan. |
| 856 40 - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://doi.org/10.1007/978-3-319-24768-7 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | eBooks |
| 264 #1 - | |
| -- | Cham : |
| -- | Springer International Publishing : |
| -- | Imprint: Springer, |
| -- | 2016. |
| 336 ## - | |
| -- | text |
| -- | txt |
| -- | rdacontent |
| 337 ## - | |
| -- | computer |
| -- | c |
| -- | rdamedia |
| 338 ## - | |
| -- | online resource |
| -- | cr |
| -- | rdacarrier |
| 347 ## - | |
| -- | text file |
| -- | |
| -- | rda |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace engineering. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Astronautics. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Multibody systems. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Vibration. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Mechanics, Applied. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Optical materials. |
| 650 #0 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Control engineering. |
| 650 14 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Aerospace Technology and Astronautics. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Multibody Systems and Mechanical Vibrations. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Optical Materials. |
| 650 24 - SUBJECT ADDED ENTRY--SUBJECT 1 | |
| -- | Control and Systems Theory. |
| 830 #0 - SERIES ADDED ENTRY--UNIFORM TITLE | |
| -- | 2193-1577 |
| 912 ## - | |
| -- | ZDB-2-ENG |
| 912 ## - | |
| -- | ZDB-2-SXE |
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