Please use this identifier to cite or link to this item:
Title: Numerical study on joined : wing aircraft
Authors: Singaravelan
Keywords: Engineering::Mechanical engineering
Issue Date: 2020
Publisher: Nanyang Technological University
Abstract: A joined wing aircraft model B150 and conventional aircraft model D150 was selected to be examined. Fluent was used to conduct Reynolds-Averaged Naiver-Stokes simulation on the aerodynamic characteristics, such as lift and drag under varied angle of attack, under transonic speed. The lift and drag coefficient were compared against different angle of attack ranging from 0°–20° degrees.The B150 model have many advantages over conventionalD150 model, discussion was done on those advantages and a study of numerical analysis on its aerodynamics was done.The comparison made between model B150 joined wing aircraft and D150 conventional aircraft indicates that a joined wing configuration is an alternative from the D150conventional aircraft.
Schools: School of Mechanical and Aerospace Engineering 
Fulltext Permission: restricted
Fulltext Availability: With Fulltext
Appears in Collections:MAE Student Reports (FYP/IA/PA/PI)

Files in This Item:
File Description SizeFormat 
FYP Report P-B028.pdf
  Restricted Access
Numerical study on joined – Wing Aircraft3.4 MBAdobe PDFView/Open

Page view(s)

Updated on Jun 18, 2024

Download(s) 50

Updated on Jun 18, 2024

Google ScholarTM


Items in DR-NTU are protected by copyright, with all rights reserved, unless otherwise indicated.