Preliminary In-Flight Boundary Layer Transition Measurements on a 45 Deg Swept Wing at Mach Numbers Between 0.9 and 1.8

By: Nasa, National Aeronautics and Space Adm

A preliminary flight experiment was flown to generate a full-scale supersonic data base to aid the assessment of computational codes, to improve instrumentation for measuring boundary layer transition... This description may be from another edition of this product.

• Format: Paperback
• Language: English
• ISBN: 1729234690
• ISBN13: 9781729234693
• Release Date: January 1
• Publisher: Independently Published
• Length: 48 Pages
• Weight: 0.30 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"