CFD analysis on sweep angles of the leading and trailing edges of a wing in a supersonic flow

CFD analysis on sweep angles of the leading and trailing edges of a wing in a supersonic flow

To systematically investigate the aerodynamic characteristics of wings with 30, 45 and 60 degree swept-back angles, and different taper ratios, Navier-Stokes (N-S) simulations for flows over a wing have been conducted. The Mach numbers of the flows range from 0.8 to 2.8. The planforms of wings are i...

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Bibliographic Details
Main Authors: Kazuya TAKEUCHI, Kisa MATSUSHIMA, Masahiro KANAZAKI, Kazuhiro KUSUNOSE
Format: Article
Language:Japanese
Published: The Japan Society of Mechanical Engineers 2015-06-01
Series:Nihon Kikai Gakkai ronbunshu
Subjects:
supersonic flow
navier-stokes simulation
wing plan-form
swept-back angle
cd-m∞ curve
Online Access:https://www.jstage.jst.go.jp/article/transjsme/81/827/81_15-00037/_pdf/-char/en

Internet

https://www.jstage.jst.go.jp/article/transjsme/81/827/81_15-00037/_pdf/-char/en

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