DSpace Repository
Structure analysis on design and fabrication of UAV capable of carrying maximum payload under given constraints
- DSpace Home
- →
- Knowledge Repository by Schools
- →
- School of Engineering
- →
- Dissertation
- →
- Under Graduate
- →
- View Item
JavaScript is disabled for your browser. Some features of this site may not work without it.
| dc.contributor.author | Gupta, Abhay | |
| dc.contributor.author | Takkar, Mangesh | |
| dc.date.accessioned | 2021-04-20T10:55:41Z | |
| dc.date.available | 2021-04-20T10:55:41Z | |
| dc.date.issued | 2013-05 | |
| dc.identifier.citation | Under the supervision of Prof. Viiav Kumar Patidar | en_US |
| dc.identifier.uri | http://hdl.handle.net/123456789/3202 | |
| dc.description | The dissertation report was submitted in partial fulfillment for the requirement of the degree of B. Tech (Aerospace Engineering) | en_US |
| dc.language.iso | en | en_US |
| dc.publisher | College of Engineering, UPES, Dehradun | en_US |
| dc.subject | Dissertation | en_US |
| dc.subject | Aerospace Engineering | en_US |
| dc.subject | Aircraft Sizing | en_US |
| dc.subject | Structural Analysis | en_US |
| dc.subject | Structural Optimization | en_US |
| dc.subject | Fabrication Scheduling | en_US |
| dc.subject | Fabrication Budgeting | en_US |
| dc.title | Structure analysis on design and fabrication of UAV capable of carrying maximum payload under given constraints | en_US |
| dc.type | Thesis | en_US |
