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INTERNATIONAL JOURNAL OF SCIENTIFIC DEVELOPMENT AND RESEARCH
International Peer Reviewed & Refereed Journals, Open Access Journal
ISSN Approved Journal No: 2455-2631 | Impact factor: 8.15 | ESTD Year: 2016
open access , Peer-reviewed, and Refereed Journals, Impact factor 8.15

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Paper Title:	TWIN FUSELAGE GLIDER LAUNCH SYSTEM
Authors Name:	Priyesh N
Unique Id:	IJSDR1701004
Published In:	Volume 2 Issue 1, January-2017
Abstract:	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.
Keywords:	UAV, Twin fuselage, V- Tail, Aspect ratio, Taper ratio
Cite Article:	"TWIN FUSELAGE GLIDER LAUNCH SYSTEM", International Journal of Science & Engineering Development Research (www.ijsdr.org), ISSN:2455-2631, Vol.2, Issue 1, page no.13 - 18, January-2017, Available :http://www.ijsdr.org/papers/IJSDR1701004.pdf
Downloads:	000346979
Publication Details:	Published Paper ID: IJSDR1701004 Registration ID:170005 Published In: Volume 2 Issue 1, January-2017 DOI (Digital Object Identifier): Page No: 13 - 18 Publisher: IJSDR \| www.ijsdr.org ISSN Number: 2455-2631

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