Optimum Design of High Speed Prop Rotors Including the Coupling of Performance, Aeroelastic Stability and Structures

By National Aeronautics and Space Administration

An optimization procedure is developed for the design of high speed prop-rotors to be used in civil tiltrotor applications. The goal is to couple aerodynamic performance, aeroelastic stability, and... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1792716656
• ISBN13: 9781792716652
• Release Date: January 1
• Publisher: Independently Published
• Length: 30 Pages
• Weight: 0.21 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"