×
INTELLIGENT WORK FORUMS
FOR ENGINEERING PROFESSIONALS

Log In

Come Join Us!

Are you an
Engineering professional?
Join Eng-Tips Forums!
  • Talk With Other Members
  • Be Notified Of Responses
    To Your Posts
  • Keyword Search
  • One-Click Access To Your
    Favorite Forums
  • Automated Signatures
    On Your Posts
  • Best Of All, It's Free!
  • Students Click Here

*Eng-Tips's functionality depends on members receiving e-mail. By joining you are opting in to receive e-mail.

Posting Guidelines

Promoting, selling, recruiting, coursework and thesis posting is forbidden.

Students Click Here

Jobs

Biplane design

Biplane design

Biplane design

(OP)
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...    

RE: Biplane design

NACA TR0458 "Relative Loading on Biplane Wings" available online from the NASA technical reports site "ntrs.nasa.gov"

Red Flag This Post

Please let us know here why this post is inappropriate. Reasons such as off-topic, duplicates, flames, illegal, vulgar, or students posting their homework.

Red Flag Submitted

Thank you for helping keep Eng-Tips Forums free from inappropriate posts.
The Eng-Tips staff will check this out and take appropriate action.

Reply To This Thread

Posting in the Eng-Tips forums is a member-only feature.

Click Here to join Eng-Tips and talk with other members!


Resources