03
Nov
06

Folding Wing Aircraft

This is a preliminary test of a proposed project to simulate the wing fluttering of an aircraft with folding wings. This was solved using the finite volume method for 3D, steady, compressible, viscous, laminar flow on a curvilinear grid. This image shows the pressure distribution over the wings.

Folding Wing Aircraft calculated in CFL3D (Computational Fluids Laboratory 3D), rendered in POV-Ray 3.6.1, 11/3/06

Links

Advertisements

0 Responses to “Folding Wing Aircraft”



  1. Leave a Comment

Leave a Reply

Fill in your details below or click an icon to log in:

WordPress.com Logo

You are commenting using your WordPress.com account. Log Out / Change )

Twitter picture

You are commenting using your Twitter account. Log Out / Change )

Facebook photo

You are commenting using your Facebook account. Log Out / Change )

Google+ photo

You are commenting using your Google+ account. Log Out / Change )

Connecting to %s


Welcome !

You will find here some of my favorite hobbies and interests, especially science and art.

I hope you enjoy it!

Subscribe to the RSS feed to stay informed when I publish something new here.

I would love to hear from you! Please feel free to send me an email : bugman123-at-gmail-dot-com

Archives

Blog Stats

  • 547,335 hits

%d bloggers like this: