Statistics: Rocket-powered model investigation of lift, drag, and stability of a body-tail configuration at Mach numbers from 0.8 to 2.3 and angles of attack between plus or minus 6.5 degrees

Context

This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and one other and was provided by UNT Libraries Government Documents Department to Digital Library, a digital repository hosted by the UNT Libraries. It has been viewed 42 times . More information about this report can be viewed below.

Usage

  • 42 Total Uses
  • 0 Uses Last 32 Days

Usage by Month/Year

Year January February March April May June July August September October November December Total
2017 0 0 0 0 0 1 0 1 0 0 0 0 2
2016 1 1 0 1 0 5 0 1 3 5 2 0 19
2015 1 0 0 0 0 0 0 0 0 0 0 2 3
2014 2 0 0 1 0 0 0 0 2 0 0 0 5
2013 0 0 0 0 0 0 1 9 0 2 0 1 13

There is no referral data available.