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Advanced BDTN inlet design for superior STOL performance in military aircraft: a computational fluid dynamics investigation

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dc.contributor.author Kumar, Syesha
dc.contributor.author Singh, Aniket Kumar
dc.contributor.author Sahu, Riya
dc.contributor.author Nagpal, Jasmeet Singh
dc.date.accessioned 2025-06-05T05:18:44Z
dc.date.available 2025-06-05T05:18:44Z
dc.date.issued 2025-05
dc.identifier.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 en_US
dc.identifier.uri https://dr.ddn.upes.ac.in//xmlui/handle/123456789/4456
dc.description Submitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering) en_US
dc.language.iso en en_US
dc.publisher School of Advanced Engineering, UPES, Dehradun en_US
dc.subject Dissertation en_US
dc.subject Aerospace Engineering en_US
dc.subject Bypass Dual Throat Nozzle en_US
dc.subject Short Take-Off and Landing en_US
dc.subject CFD Investigation en_US
dc.subject Military STOL Aircraft en_US
dc.subject Thrust Vectoring en_US
dc.subject Lift Enhancement en_US
dc.title Advanced BDTN inlet design for superior STOL performance in military aircraft: a computational fluid dynamics investigation en_US
dc.type Other en_US


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