International Journal of Application or Innovation in Engineering & Management
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ISSN 2319 – 4847
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Call for Paper, Published Articles, Indexing Infromation A Study and Design Of Scramjet Engine Inlet By Using Computational Fluid Dynamics Analysis, Authors : Kalyan Dagamoori , Sruthi Bobba , V.N.Sai Kiran Aka , Kavali Rakesh , Md .Abdul Sami, Sumama Yaqub Ali , R.Sahiti , Kosaraju Shreya, International Journal of Application or Innovation in Engineering & Management (IJAIEM), www.ijaiem.org
Volume & Issue no: Volume 4, Issue 6, June 2015

Title:
A Study and Design Of Scramjet Engine Inlet By Using Computational Fluid Dynamics Analysis
Author Name:
Kalyan Dagamoori , Sruthi Bobba , V.N.Sai Kiran Aka , Kavali Rakesh , Md .Abdul Sami, Sumama Yaqub Ali , R.Sahiti , Kosaraju Shreya
Abstract:
ABSTRACT Generally a Scramjet Engine starts at a hypersonic freestream physicist no. 5.00. so as to propel to those speeds, we have a tendency to use turbojet engines that propel to around 3.00-4.00 physicistand from there the athodyd picks upon and starts to propel to begin the scramjet engine. If we have a tendency to cut back the scramjet engine beginning ratio to mention 3.50 or 4.00, we are able toeliminate one propulsion engine, i.e., atherodyde and so reducing weight and quality. the planning for such a scramjet engine is meted out during this project considering solely the water styles and therefore the flow analysis is meted out in CFD. A 2 dimensional analysis is meted out during thisproject. GAMBIT is employed to make a model. FLUENT is employed to hide the flow analysis. Keywords : CFD Analysis , Combustion , Supersonic Exhaust , Exhaust flow , Free stream flow , Scramjet Engine ,Oblique Shockwave System.
Cite this article:
Kalyan Dagamoori , Sruthi Bobba , V.N.Sai Kiran Aka , Kavali Rakesh , Md .Abdul Sami, Sumama Yaqub Ali , R.Sahiti , Kosaraju Shreya , " A Study and Design Of Scramjet Engine Inlet By Using Computational Fluid Dynamics Analysis " , International Journal of Application or Innovation in Engineering & Management (IJAIEM), Volume 4, Issue 6, June 2015 , pp. 017-030 , ISSN 2319 - 4847.
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