Development and performance evaluation of the flapping wing with In-situ piezoceramic actuator (Record no. 429585)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 02012nam a22002297a 4500 |
| 008 - FIXED-LENGTH DATA ELEMENTS--GENERAL INFORMATION | |
| fixed length control field | 230719b |||||||| |||| 00| 0 eng d |
| 041 ## - LANGUAGE CODE | |
| Language code of text/sound track or separate title | en |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 620 |
| Item number | BHU |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Nagarajan, Bhuvana |
| 245 ## - TITLE STATEMENT | |
| Title | Development and performance evaluation of the flapping wing with In-situ piezoceramic actuator |
| 260 ## - PUBLICATION, DISTRIBUTION, ETC. (IMPRINT) | |
| Place of publication, distribution, etc | Bangalore : |
| Name of publisher, distributor, etc | IISc , |
| Date of publication, distribution, etc | 2023 . |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | xxi, 154p. |
| Other physical details | col. ill. ; |
| Dimensions | 29.1 cm * 20.5 cm |
| Accompanying material | e-Thesis |
| Size of unit | 6.196Mb |
| 500 ## - GENERAL NOTE | |
| General note | include bibliographic reference and index |
| 502 ## - DISSERTATION NOTE | |
| Dissertation note | PhD; 2023; Centre for nano science and engineering |
| 520 ## - SUMMARY, ETC. | |
| Summary, etc | Unmanned Aerial Vehicles (UAV) are essentially automatic flight vehicles having dimensions, wingspan and airspeed, smaller than the conventional aerial vehicles. UAVs are employed widely in applications such as surveillance over a short distance, acquisition of a local target, detection of hazardous chemicals / biological agent, exploration of a harmful environment, search operations, etc. UAV can be classified into three main types depending on their method of propulsion and lift. These are fixed wing, rotary wing, and flapping wing. Flapping wing UAVs are more suitable for insect scale flights. Flapping mechanism requires actuators with large stroke periodic (reciprocal) motion at high speed (10-100s of Hz) with large output forces for overcoming the aerodynamic damping. There are several actuation mechanisms applicable to flapping-wing UAVs. The emphasis is on linear actuators, which simplify the mechanical transmission for flapping motions. Most of the prototypes developed so far have employed motor-driven mechanisms to achieve the flapping wing. Unconventional methods such as piezoelectric, thermal, electromagnetic, shape memory, electrostatic, etc. for actuation of flapping wings have also been used. |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | Unmanned Aerial Vehicles |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | flapping wing |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name as entry element | piezoelectric actuator |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Pratap, Rudra advised |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | https://etd.iisc.ac.in/handle/2005/6156 |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Koha item type | Thesis |
| Withdrawn status | Lost status | Source of classification or shelving scheme | Damaged status | Not for loan | Home library | Current library | Date acquired | Total Checkouts | Full call number | Barcode | Date last seen | Koha item type |
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| Dewey Decimal Classification | JRD Tata Memorial Library | JRD Tata Memorial Library | 19/07/2023 | 620 BHU | ET00169 | 19/07/2023 | E-BOOKS |
