Advanced BDTN inlet design for superior STOL performance in military aircraft: a computational fluid dynamics investigation
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School of Advanced Engineering, UPES, Dehradun
Abstract
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Submitted in the partial fulfillment of the requirement for the degree of B. Tech (Aerospace Engineering)
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