Statistics: Investigation of a High-Pressure-Ratio Eight-Stage Axial-Flow Research Compressor With Two Transonic Inlet Stages 1: Aerodynamic Design

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 340 times , with 4 in the last month . More information about this report can be viewed below.

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Year January February March April May June July August September October November December Total
2019 2 4 6
2018 7 12 16 4 7 6 2 8 2 1 8 7 80
2017 12 2 0 5 7 8 2 13 10 18 5 16 98
2016 2 4 2 6 2 9 12 7 13 10 24 11 102
2015 0 3 0 0 1 0 0 0 0 1 2 4 11
2014 3 1 0 0 3 1 9 2 1 6 2 0 28
2013 0 0 1 0 2 0 10 1 0 0 0 0 14
2012 1 0 0 0 0 0 0 0 0 0 0 0 1

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