Please use this identifier to cite or link to this item:
https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4456| Title: | Advanced BDTN inlet design for superior STOL performance in military aircraft: a computational fluid dynamics investigation |
| Authors: | Kumar, Syesha Singh, Aniket Kumar Sahu, Riya Nagpal, Jasmeet Singh |
| Keywords: | Dissertation Aerospace Engineering Bypass Dual Throat Nozzle Short Take-Off and Landing CFD Investigation Military STOL Aircraft Thrust Vectoring Lift Enhancement |
| Issue Date: | May-2025 |
| Publisher: | School of Advanced Engineering, UPES, Dehradun |
| Citation: | Under the guidance of Mr. Ramesh Kumar, Project Supervisor, UPES ; Dr. Harshit Shukla, Project Co-supervisor, UPES and Dr. Ram Kunwer, Activity Coordinator, UPES |
| Description: | Submitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering) |
| URI: | https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4456 |
| Appears in Collections: | Under Graduate |
Files in This Item:
| File | Description | Size | Format | |
|---|---|---|---|---|
| Advanced_BDTN_Inlet_Design_for_Superior_STOL_Performance_in_Military_Aircraft__A_Computational_Fluid_D - Syesha Kumar.pdf | 8.84 MB | Adobe PDF | View/Open |
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