FLOW VARIATION OVER BI-CONIC NOSE PROFILE AT DIFFERENT ANGLE OF ATTACK
Angle of Attack (AOA), Mach Number , Nose cone, Drag, CFD
The object moving at high speed induced the drag which decrease the velocity and affect the efficiencies of object .Now days we are moving towards the high speed vehicle. By the high speed vehicle we save our time and more accurate on trget like in defence system we use the different ballistic missile for targeting the object .In Aerospace Industries the main problem is drag and some time is usefull for us like example in re-entry of object to the earth atmosphere .In that situation we want more drag and less lift. Designing field give the ability to make more efficient body design for Aerospace Industry .By which we tackle the decelrate problem in moving object.The motivation for such a work is caused by lack of data on aerodynamic profile for biconic nose cone. This paper deals with computational analysis on biconic nose cone design profile for rocket and missiles. The effect of nose shape on the drag is studied at sonic level its mean that the object should move with the mach1.0 at velocity of 343m/sec .The scope of this paper develop projects on satellite mssion rockets and increasing their efficiency and effect on target also. By this paper we develop prototype profile with accurate aerodynamics. It also represent the variation of lift,drag with different angle of attack.
"FLOW VARIATION OVER BI-CONIC NOSE PROFILE AT DIFFERENT ANGLE OF ATTACK", IJSDR - International Journal of Scientific Development and Research (www.IJSDR.org), ISSN:2455-2631, Vol.5, Issue 9, page no.200 - 205, September-2020, Available :https://ijsdr.org/papers/IJSDR2009033.pdf
Volume 5
Issue 9,
September-2020
Pages : 200 - 205
Paper Reg. ID: IJSDR_192459
Published Paper Id: IJSDR2009033
Downloads: 000347207
Research Area: Engineering
Country: Delhi, delhi, India
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
