ansys/fluent-14 code (ANSYS inc)
90
Structured Review
ANSYS inc
ansys/fluent-14 code
Ansys/Fluent 14 Code, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
https://www.bioz.com/product/14-fluent+code/ansys+fluent+14+0+code/10__1134_slash_s0040601523030072-166-51-51
Average 90 stars, based on 1 article reviews
Ansys/Fluent 14 Code, supplied by ANSYS inc, used in various techniques. Bioz Stars score: 90/100, based on 1 PubMed citations. ZERO BIAS - scores, article reviews, protocol conditions and more
https://www.bioz.com/product/14-fluent+code/ansys+fluent+14+0+code/10__1134_slash_s0040601523030072-166-51-51
Average 90 stars, based on 1 article reviews
ansys/fluent-14 code - by Bioz Stars,
2026-09
90/100 stars
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other:Article Title: Effect of variation of angle of attack on the performance of two-strut scramjet combustor Article Snippet: Computational simulation of Scramjet combustor at Mach 2.5 through two struts and with three angle of attack (a 1⁄4 3 , a 1⁄4 0 and a 1⁄4 3 ) have been presented and discussed in the present research article.. Here the fuel which is injected through two struts is placed parallel to the air stream.. The geometry and model used here is slight modification of the DLR (German Aerospace Center) scramjet model. Article Title: Investigation on the effects of operating variables on the performance of two-strut scramjet combustor Article Snippet: The two equation SST k u turbulence model and the two-dimensional compressible Reynolds-Averaged NaviereStokes (RANS) equations along with single-step chemical reaction mechanism have been applied to analyze the effect of divergence angle, radius of the strut tip and the half angle of the strut on the combustion enhancement of two-strut scramjet combustor.. Here all the simulations are carried out by using ANSYS 14-FLUENT code.. Simultaneously, the validation of the present computational simulation for single strut injection has been completed by comparing its result with the available DLR experimental data which is available in the literature. |