Marine Solutions Aerospace Solutions Automotive Solutions
| Overview | | High Lift Validation | | Compressibility Validation | | Unsteady Validation(1) | | Unsteady Validation(2) | | Low AR Validation | | Low AR Validation(2) |
Here, NEWPAN is compared against NASA experimental data.
John W. Boyd, "Aerodynamic characteristics of two 25-percent-area trailing-edge flaps on an aspect ratio 2 triangular wing at subsonic and supersonic speeds" - NASA RM A52D01c, 1952

Results for Cl, Cd, Cm are shown for an incidence sweep, for different flap angle deflections





[Home] [Products] [Solutions] [About Us] [Contact Us] [Support] [Site Map]

Copyright © 2019 Flow Solutions Ltd.  All rights reserved. 
Company Registration No 2010440, Registered Office 61 Grace Close Chipping Sodbury, South Glos BS37 6ND