TWIN FUSELAGE GLIDER LAUNCH SYSTEM

Priyesh N

UAV, Twin fuselage, V- Tail, Aspect ratio, Taper ratio

In order to improve the payload capability, reduce the bending moments and launch mini rockets and weather balloons, the development of a twin fuselage configuration glider launch system is introduced in our project. Twin fuselage configuration is considered to be advantageous in both aerodynamics and structures. Through this project we evaluate the possibilities for future full-scale aircraft. The flight performance and stability are evaluated by flight test.

Published Paper   E-Certificate

"TWIN FUSELAGE GLIDER LAUNCH SYSTEM", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.2, Issue 1, page no.13 - 18, January-2017, Available :https://ijsdr.org/papers/IJSDR1701004.pdf

Volume 2 Issue 1, January-2017

Pages : 13 - 18

Paper Reg. ID: IJSDR_170005

Published Paper Id: IJSDR1701004

Downloads: 000347092

Research Area: Engineering

Country: KASARAGOD, KERALA, India

Published Paper PDF: https://ijsdr.org/papers/IJSDR1701004

Published Paper URL: https://ijsdr.org/viewpaperforall?paper=IJSDR1701004

ISSN: 2455-2631 | IMPACT FACTOR: 9.15 Calculated By Google Scholar | ESTD YEAR: 2016

An International Scholarly Open Access Journal, Peer-Reviewed, Refereed Journal Impact Factor 9.15 Calculate by Google Scholar and Semantic Scholar | AI-Powered Research Tool, Multidisciplinary, Monthly, Multilanguage Journal Indexing in All Major Database & Metadata, Citation Generator

Publisher: IJSDR(IJ Publication) Janvi Wave

This work is licensed under a Creative Commons Attribution 4.0 International License and The Open Definition