Search

Search U.S. government technical reports digitized or harvested by TRAIL.

Keyword Search

Enter your search term(s):
[advanced search]

2 results returned

Search results

• Effects of an inset tab on the hinge-moment and effectiveness characteristics of an unswept trailing-edge control on a 60©� delta wing at Mach numbers from 0.75 to 1.96
• Flight investigation of a small side-located control stick used with electronic control systems in a fighter airplane