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

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dc.contributor.authorKumar, Syesha
dc.contributor.authorSingh, Aniket Kumar
dc.contributor.authorSahu, Riya
dc.contributor.authorNagpal, Jasmeet Singh
dc.date.accessioned2025-06-05T05:18:44Z
dc.date.available2025-06-05T05:18:44Z
dc.date.issued2025-05
dc.descriptionSubmitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering)en_US
dc.identifier.citationUnder the guidance of Mr. Ramesh Kumar, Project Supervisor, UPES ; Dr. Harshit Shukla, Project Co-supervisor, UPES and Dr. Ram Kunwer, Activity Coordinator, UPESen_US
dc.identifier.urihttps://dr.ddn.upes.ac.in/handle/123456789/4456
dc.language.isoenen_US
dc.publisherSchool of Advanced Engineering, UPES, Dehradunen_US
dc.subjectDissertationen_US
dc.subjectAerospace Engineeringen_US
dc.subjectBypass Dual Throat Nozzleen_US
dc.subjectShort Take-Off and Landingen_US
dc.subjectCFD Investigationen_US
dc.subjectMilitary STOL Aircraften_US
dc.subjectThrust Vectoringen_US
dc.subjectLift Enhancementen_US
dc.titleAdvanced BDTN inlet design for superior STOL performance in military aircraft: a computational fluid dynamics investigationen_US
dc.typeOtheren_US

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