Statistics: Investigation of the effects of leading-edge flaps on the aerodynamic characteristics in pitch at Mach numbers from 0.40 to 0.93 of a wing-fuselage configuration with a 45 degree sweptback wing of aspect ratio 4

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 36 times . More information about this report can be viewed below.

Usage

  • 36 Total Uses
  • 0 Uses Last 30 Days

Usage by Month/Year

Year January February March April May June July August September October November December Total
2018 0 0 1 0 0 0 0 0 0 1
2017 0 0 0 0 0 0 0 1 0 0 0 0 1
2016 0 0 0 0 0 1 0 0 0 1 0 0 2
2014 1 0 2 1 0 0 0 0 0 0 0 0 4
2013 0 1 1 0 0 0 0 18 7 0 1 0 28

There is no referral data available.