Please use this identifier to cite or link to this item:
http://13.232.72.61:8080/jspui/handle/123456789/9775Full metadata record
| DC Field | Value | Language |
|---|---|---|
| dc.date.accessioned | 2025-09-22T05:58:06Z | - |
| dc.date.available | 2025-09-22T05:58:06Z | - |
| dc.date.issued | 2025-07 | - |
| dc.identifier.uri | http://13.232.72.61:8080/jspui/handle/123456789/9775 | - |
| dc.language.iso | en | en_US |
| dc.publisher | VTU | en_US |
| dc.subject | Aeronautical engineering | en_US |
| dc.subject | Question Papers | en_US |
| dc.subject | 5th Sem | en_US |
| dc.title | Aeronautical Engineering June-July 2025 | en_US |
| dc.type | Other | en_US |
| Appears in Collections: | June-July 2025 | |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Aero Structures-21AE53.pdf | 1.69 MB | Adobe PDF | View/Open | |
| Aircraft Performance and Stability- 21AE-AS54.pdf | 1.09 MB | Adobe PDF | View/Open | |
| Aircraft Propulsion-21AE52.pdf | 1.27 MB | Adobe PDF | View/Open | |
| Aircraft structures- BAE502.pdf | 2.03 MB | Adobe PDF | View/Open | |
| Aviation Management- BAE-BAS501.pdf | 805.91 kB | Adobe PDF | View/Open | |
| Finite Elements Methods-BAE-BAS515A.pdf | 2.04 MB | Adobe PDF | View/Open | |
| Heat and Mass Transfer - 17AE53.pdf | 1.27 MB | Adobe PDF | View/Open | |
| Mechanism and Machine Theory- 21AE-AS51.pdf | 1.63 MB | Adobe PDF | View/Open | |
| Unmanned Aerial Vechicles- Basic and Applications-BAE503.pdf | 704.8 kB | Adobe PDF | View/Open |
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