A two dimensional study of rotor/airfoil interaction in hover

By: Nasa, National Aeronautics and Space Adm

A two dimensional model for the chordwise flow near the wing tip of the tilt rotor in hover is presented. The airfoil is represented by vortex panels and the rotor is modeled by doublet panels. The... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1729075398
• ISBN13: 9781729075395
• Release Date: January 1
• Publisher: Independently Published
• Length: 40 Pages
• Weight: 0.26 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"