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

• Free-flight measurements of aerodynamic heat transfer to Mach number 3.9 and of drag to Mach number 6.9 of a fin-stabilized cone-cylinder configuration
• Aerodynamic characteristics in pitch of several triple-body missile configurations at Mach numbers 0.6 to 1.4