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Paper Information

Journal:   JOURNAL OF APPLIED FLUID MECHANICS (JAFM)   2016 , Volume 9 , Number 3; Page(s) 1215 To 1220.
 
Paper: 

NUMERICAL INVESTIGATION ON HYDROGEN-FUELED SCRAMJET COMBUSTOR WITH PARALLEL STRUT FUEL INJECTOR AT A FLIGHT MACH NUMBER OF 6

 
 
Author(s):  PANDEY K.M.*, ROGA S., CHOUBEY G.
 
* DEPARTMENT OF MECHANICAL ENGINEERING, NATIONAL INSTITUTE OF TECHNOLOGY SILCHAR, ASSAM, INDIA
 
Abstract: 

A numerical analysis of the inlet-combustor interaction and flow structure through a scramjet engine at a flight Mach number M=6 with parallel injection (Strut with circular inlet) is presented in the present research article. Three different angles of attack (a=-4o, a =0o a =4o) have been studied for parallel injection.
The scramjet configuration used here is a modified version of DLR scramjet model. Fuel is injected at supersonic speed (M=2) through a parallel strut injector. For parallel injection, the shape of the strut is chosen in a way to produce strong stream wise vorticity and thus to enhance the hydrogen/air mixing inside the combustor. These numerical simulations are aimed to study the flow structure, supersonic mixing, and combustion phenomena for the three different types of geometries along with circular shaped strut configuration.

 
Keyword(s): SCRAMJET, HYPERSONIC COMBUSTION, K?ε REALIZABLE MODEL, PARALLEL INJECTOR
 
 
References: 
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Click to Cite.
APA: Copy

PANDEY, K., & ROGA, S., & CHOUBEY, G. (2016). NUMERICAL INVESTIGATION ON HYDROGEN-FUELED SCRAMJET COMBUSTOR WITH PARALLEL STRUT FUEL INJECTOR AT A FLIGHT MACH NUMBER OF 6. JOURNAL OF APPLIED FLUID MECHANICS (JAFM), 9(3), 1215-1220. https://www.sid.ir/en/journal/ViewPaper.aspx?id=571019



Vancouver: Copy

PANDEY K.M., ROGA S., CHOUBEY G.. NUMERICAL INVESTIGATION ON HYDROGEN-FUELED SCRAMJET COMBUSTOR WITH PARALLEL STRUT FUEL INJECTOR AT A FLIGHT MACH NUMBER OF 6. JOURNAL OF APPLIED FLUID MECHANICS (JAFM). 2016 [cited 2021May15];9(3):1215-1220. Available from: https://www.sid.ir/en/journal/ViewPaper.aspx?id=571019



IEEE: Copy

PANDEY, K., ROGA, S., CHOUBEY, G., 2016. NUMERICAL INVESTIGATION ON HYDROGEN-FUELED SCRAMJET COMBUSTOR WITH PARALLEL STRUT FUEL INJECTOR AT A FLIGHT MACH NUMBER OF 6. JOURNAL OF APPLIED FLUID MECHANICS (JAFM), [online] 9(3), pp.1215-1220. Available: https://www.sid.ir/en/journal/ViewPaper.aspx?id=571019.



 
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