Statistics: Effects of Plan Form, Airfoil Section, and Angle of Attack on the Pressures Along the Base of Blunt-Trailing-Edge Wings at Mach Numbers of 1.41, 1.62, and 1.96

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

Usage

  • 93 Total Uses
  • 0 Uses Last 35 Days

Usage by Month/Year

Year January February March April May June July August September October November December Total
2018 2 0 1 0 0 2 0 3 0 8
2017 1 0 0 0 1 0 0 1 2 4 3 1 13
2016 0 0 1 3 0 3 0 0 0 2 1 2 12
2015 0 0 0 2 1 1 0 0 0 1 2 0 7
2014 1 0 0 0 2 0 2 2 4 1 0 0 12
2013 0 1 0 0 0 0 14 23 0 0 1 1 40
2012 0 0 0 0 0 0 0 0 0 1 0 0 1

There is no referral data available.