Integrated Aerodynamic/Dynamic Optimization of Helicopter Rotor Blades

By National Aeronautics and Space Administration

An integrated aerodynamic/dynamic optimization procedure is used to minimize blade weight and 4 per rev vertical hub shear for a rotor blade in forward flight. The coupling of aerodynamics and... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1792652852
• ISBN13: 9781792652851
• Release Date: January 1
• Publisher: Independently Published
• Length: 32 Pages
• Weight: 0.22 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"