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

• Investigations at supersonic speeds of 22 triangular wings representing two airfoil sections for each of 11 apex angles
• Investigation of spoiler ailerons for use as speed brakes or glide-path controls on two NACA 65-series wings equipped with full-span slotted flaps