Analysis of Low Speed Aerodynamics of Double Delta Wing
Swaraj Singh, jayanta sinha
Cite This Article:
Analysis of Low Speed Aerodynamics of Double Delta WingInternational Journal of Innovative Research in Technology( ,ISSN: 2349-6002 ,Volume 6 ,Issue 6 ,Page(s):196-202 ,November 2019 ,Available :IJIRT148816_PAPER.pdf
computational fluid dynamics, double delta wing, turbulence models, subsonic, hypersonic
Wilbur Wright has famously noted that “The desire of flying is an idea handed down to us by our ancestors who looked enviously on the birds soaring freely through space on the infinite highway of the air.” My paper addresses that curiosity of finding out the flow around a flying object, here, in this research work, double delta wing. In this research work, numerical as well as experimental investigation was performed on 80/56.867-deg double-delta wing to obtain lift and drag coefficients. Low speed aerodynamics was analyzed on this type of wing configuration. For the double-delta wing study, both numerical and experimental investigation was carried out, and the results from both numerical and experimental predications were compared to the experimental data found in existing literature. “The results of the comparison of lift and drag coefficients show good agreement with the experiments.” In general, “the comparison shows good agreement” with the different CFD predictions as well as experimental studies and theoretical calculations.
Article Details
Unique Paper ID: 148816

Publication Volume & Issue: Volume 6, Issue 6

Page(s): 196 - 202
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Last Date 25 January 2020

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