Aeronautic Engineers

  
Home | Aircraft engineering | other topics | Rotorcraft engineering
  Position：HOME>Aerodynamic engineering>Article Content
Biplane design
Source：Internet Author：Unknow Pubdate：2008-10-30  
tobyskywalker (Aeronautics) 20 Jun 08 10:07
Hi everyone!

I'm truly involve with the design of biplanes but I have got a big problem, does anyone knows how to calculate the wing lift slope of a biplane configuration?

Does any one knows how to calculate it according the stagger, decalage or gap, or even with the Munk's factor?

Because right now I'm using the non lifting line theory equations of prandtl.. but these are for monoplanes!.

Thank you, I need help urgent...    

rb1957 (Aerospace) 20 Jun 08 10:24
NACA TR0458 "Relative Loading on Biplane Wings" available online from the NASA technical reports site "ntrs.nasa.gov"

（Click：）

Previous：I need an MSDS for Brayco 350   Next：ground and surface effect sources?
[Add TO Favorites] [TOP] [PRINT] [CLOCE WINDOWS]  
  Hot Article
·2d Fluent and Airfoil
·Ultralight airfoil
·US air force DATCOM
·Wind Tunnel Smoke Generator
·Freeware 2d/3d airfoil calcula
·Multi-element high lift wing f
·fenders vs. no fenders
·What is optimum number of prop
·NACA AIRFOIL
·vortex lattice method - drag
·VAWT Flat plane formula
·Bicycle fairing design in wind
  Related Articles
·ground and surface effect sour
·Custer Channelwing
·Vertical axis windmill questio
·Max Range vs Max Endurance
·High speed trains - tunnels
·Mach 0,3 across the entrance o
·Efficiecy of Cooling Tower Fan
·Ducted fan design software fro
·Is it possible? Helicopter bla
·Vertical Flight
·Split-ailerons, need help unde
·Why flags flutter
Power by DedeCms