Analysis of Flapping Wings Micro Air Vehicle / (Record no. 609206)
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| 000 -LEADER | |
|---|---|
| fixed length control field | 01423nam a22001577a 4500 |
| 082 ## - DEWEY DECIMAL CLASSIFICATION NUMBER | |
| Classification number | 621 |
| 100 ## - MAIN ENTRY--PERSONAL NAME | |
| Personal name | Attiq ur Rehman, Muhammad |
| 245 ## - TITLE STATEMENT | |
| Title | Analysis of Flapping Wings Micro Air Vehicle / |
| Statement of responsibility, etc. | Muhammad Attiq ur Rehman |
| 264 ## - PRODUCTION, PUBLICATION, DISTRIBUTION, MANUFACTURE, AND COPYRIGHT NOTICE | |
| Place of production, publication, distribution, manufacture | Islamabad : |
| Name of producer, publisher, distributor, manufacturer | SMME- NUST; |
| Date of production, publication, distribution, manufacture, or copyright notice | 2022. |
| 300 ## - PHYSICAL DESCRIPTION | |
| Extent | 68p. |
| Other physical details | Soft Copy |
| Dimensions | 30cm |
| 500 ## - GENERAL NOTE | |
| General note | Flapping Wings Micro Air Vehicles (MAVs) are incredible flyers. It is evident from the literature that flapping wings micro air vehicles have higher lift to drag ratio and higher power to weight ratio. Current study aims to dug in the effects of flapping frequency, flapping angle, and velocity and in phase verses out of phase motion of Fore and Hindwings on the basic aerodynamic coefficients. Numerical Simulations in ANSYS Fluent have been performed on the approximate 3D CAD Model of Dragonfly made in SolidWorks. The results show that L/D ratio is maximum for the cases with Low Velocities, Higher Flapping Frequencies and Higher Flapping Angles. L/D Ratio for In phase motion of wings at low velocity is higher and higher for Out of phase motion at high velocity provided same Flapping Frequency, and Flapping Angle. L/D ratio is higher for 25° Flapping Angle/Angle of Attack for most cases. |
| 650 ## - SUBJECT ADDED ENTRY--TOPICAL TERM | |
| Topical term or geographic name entry element | MS Mechanical Engineering |
| 700 ## - ADDED ENTRY--PERSONAL NAME | |
| Personal name | Supervisor : Dr. Emad Uddin |
| 856 ## - ELECTRONIC LOCATION AND ACCESS | |
| Uniform Resource Identifier | <a href="http://10.250.8.41:8080/xmlui/handle/123456789/29399">http://10.250.8.41:8080/xmlui/handle/123456789/29399</a> |
| 942 ## - ADDED ENTRY ELEMENTS (KOHA) | |
| Source of classification or shelving scheme | |
| Koha item type | Thesis |
| Withdrawn status | Permanent Location | Current Location | Shelving location | Date acquired | Full call number | Barcode | Koha item type |
|---|---|---|---|---|---|---|---|
| School of Mechanical & Manufacturing Engineering (SMME) | School of Mechanical & Manufacturing Engineering (SMME) | E-Books | 05/21/2024 | 621 | SMME-TH-701 | Thesis |