Design and Development of Rukma Vimana Nozzle
M. Prashanth Reddy1, V V S H Prasad2, G.V.R.Seshagiri Rao3, C.Labesh Kumar4
1M. Prashanth Reddy*, Assistant professor, Mechanical Engineering, Institute of Aeronautical Engineering College, Hyderabad, India.
2Prof. V V S H Prasad Professor, Mechanical Engineering, Institute of aeronautical Engineering college, Hyderabad, India.
3Dr.G.V.R.Seshagiri Rao, Professor, Mechanical Engineering, Institute of aeronautical Engineering college, Hyderabad, India.
4C.Labesh Kumar, Assistant Professor, Mechanical Engineering, Institute of aeronautical Engineering college, Hyderabad, India.
Manuscript received on December 16, 2019. | Revised Manuscript received on December 22, 2019. | Manuscript published on January 10, 2020. | PP: 793-796 | Volume-9 Issue-3, January 2020. | Retrieval Number: L32201081219/2020©BEIESP | DOI: 10.35940/ijitee.L3220.019320
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© The Authors. Blue Eyes Intelligence Engineering and Sciences Publication (BEIESP). This is an open access article under the CC BY-NC-ND license (http://creativecommons.org/licenses/by-nc-nd/4.0/)
Abstract: Rukma vimana is a part extraction from vimana Shastra. This project deals with nozzle system of ancient rukma vimana for vertical take-off systems. Nozzle design is very important to provide the necessary lift to the vimana. In the vimana Shastra a provision has been identified to create external heat supply to the streamed flow system in nozzle. In the present work external heat is applied to the nozzle section and to estimate the coefficient of lift. An attempt is being made to create CAD modelling and perform ANSYS fluent analysis to validate theoretical correlations. Keywords: Bumper, dynamic and modal analysis,
Keywords: In the Present Work External heat is Applied to the Nozzle Section and to Estimate the Coefficient of lift.
Scope of the Article: Recent Trends & Developments in Computer Networks