Effects of Swept Tips on V-22 Whirl Flutter and Loads

By National Aeronautics and Space Administration

Technical Report Acree, C. W., Jr. Ames Research Center NASA/TM-2005-213458, A-0513650 WBS 21-745-00-00 ROTOR AERODYNAMICS; TILT ROTOR AIRCRAFT; V-22 AIRCRAFT; STABILITY; LOADS (FORCES); FLUTTER; WAKES

• Format: Paperback
• Language: English
• ISBN: B08F6YD6R1
• ISBN13: 9798673113394
• Release Date: January 1
• Publisher: Independently Published
• Length: 50 Pages
• Weight: 0.31 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"