A Study of the Vortex Flow Over 76/40-Deg Double-Delta Wing

By: Nasa, National Aeronautics and Space Adm

A low-speed wind-tunnel study of the flow about a 76/40-deg double-delta wing is described for angles of attack ranging from -10 to 25 deg and Reynolds numbers ranging from 0.5 to 1.5 Million. The... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1729072704
• ISBN13: 9781729072707
• Release Date: January 1
• Publisher: Independently Published
• Length: 40 Pages
• Weight: 0.26 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"