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

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PANDEY K.M.; ROGA S.; CHOUBEY G.

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Journal Paper

Paper Information

Journal: JOURNAL OF APPLIED FLUID MECHANICS (JAFM) Year:2016 | Volume:9 | Issue:3 Page(s): 1215-1220

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Title

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. | Issue Writer Certificate

Keywords

SCRAMJET

HYPERSONIC COMBUSTION

K−ε REALIZABLE MODEL

PARALLEL INJECTOR

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.

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APA: Copy

PANDEY, K.M., 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. SID. https://sid.ir/paper/307742/en

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)[Internet]. 2016;9(3):1215-1220. Available from: https://sid.ir/paper/307742/en

IEEE: Copy

K.M. PANDEY, S. ROGA, and G. CHOUBEY, “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), vol. 9, no. 3, pp. 1215–1220, 2016, [Online]. Available: https://sid.ir/paper/307742/en

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