 |
 |
 |
|
|
|
[Sponsors] | ||||
July 27, 2020, 16:31
|
CL for bi wing
|
#1 |
|
Member
Thu Win
Join Date: Apr 2017
Posts: 70
Rep Power: 9  |
Is the CL for biwing L/(.5 rho * V^2 *2s)?
|
|
|
|
|
|
December 20, 2020, 02:01
|
|
#2 |
|
Senior Member
Kira
Join Date: Nov 2020
Location: Canada
Posts: 435
Rep Power: 8 |
Hello,
No, the formula for the lift coefficient is more complex for the wing of a biplane. It also depends if they are staggered or not. Here is a report by Max Munk courtesy of NASA that goes over biplane theory: https://ntrs.nasa.gov/api/citations/...9930091216.pdf |
|
|
|
|
|
 |
|
|
Similar Threads
|
||||
| Thread | Thread Starter | Forum | Replies | Last Post |
| Ffd_control_point_2d | feiyi | SU2 | 4 | September 30, 2019 12:42 |
| [ANSYS Meshing] Meshing fluid around sharp edges of a 3D insect wing. | minglis | ANSYS Meshing & Geometry | 1 | February 2, 2017 09:14 |
| Wing FSI simulation: Shell elements or 3D solid body? | frossi | CFX | 3 | June 15, 2016 20:02 |
| Using the wing mesher | GavinB | STAR-CCM+ | 1 | November 20, 2015 01:14 |
| [ICEM] Blocking For Swept Wing | air_engineer_arsenal | ANSYS Meshing & Geometry | 13 | July 24, 2012 11:52 |
1Likes
Linear Mode
