Design and Analysis of Double Bobble Cross Section Fuselage Micro-Class Aircraft
M.Satyanarayana Gupta1, Kalavagunta Veeranjaneyulu2, MNVS Swetha Bala3
1M.Satyanarayana Gupta, Professor, Department of Aeronautical Engineering, MLR Institute of Technology, Hyderabad, India.
2K.Veeranjaneyulu, Professor, Department of Aeronautical Engineering MLR Institute of technology, Hyderabad, India.
3MNVS Swetha Bala, Associate Professor, Department of Aeronautical Engineering, MLR Institute of technology, Hyderabad, India.
Manuscript received on November 17., 2019. | Revised Manuscript received on November 24 2019. | Manuscript published on 30 November, 2019. | PP: 12200-12202 | Volume-8 Issue-4, November 2019. | Retrieval Number: D9133118419/2019©BEIESP | DOI: 10.35940/ijrte.D9133.118419
Open Access | Ethics and Policies | Cite | Mendeley | Indexing and Abstracting
© 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: The applications of micro-class aircraft is increasing day by day and all industrial community which depending on mobility and surveillance are accepting this type of aircrafts. The main objective of this work is to design and fabricate an aircraft that is capable to carry the highest payload fraction possible with lowest empty weight fraction which all industries required today. Bobble Cross Section Fuselage Micro-Class Aircraft carriers more pay load with maximum lift, minimum airplane weight and drag.
Keywords: UAV, Micro-Class Aircraft, Double Bobble Fuselage
Scope of the Article: Predictive Analysis.