Modal Correction Method For Dynamically Induced Errors In Wind-Tunnel Model Attitude Measurements

By: Nasa, National Aeronautics and Space Adm

This paper describes a method for correcting the dynamically induced bias errors in wind tunnel model attitude measurements using measured modal properties of the model system. At NASA Langley... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 179268715X
• ISBN13: 9781792687150
• Release Date: January 1
• Publisher: Independently Published
• Length: 28 Pages
• Weight: 0.20 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"