naca-tn-1696

Version
0 Downloads
0.00 KB File Size
0 File Count
December 6, 2016 Create Date
December 6, 2016 Last Updated

▼ Scroll for Details ▼

National Advisory Committee for Aeronautics, Technical Notes - Chordwise Pressure Distributions on a 12' Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60

naca-tn-1696-chordwise-pressure-distributions-on-a-12-span-wing-of-naca-66-series-airfoil-sections-up-to-a-mach-number-of-0-60-1

Comment On This Post Cancel reply

naca-tn-1696

Version
0 Downloads
0.00 KB File Size
0 File Count
December 6, 2016 Create Date
December 6, 2016 Last Updated

▼ Scroll for Details ▼

National Advisory Committee for Aeronautics, Technical Notes - Chordwise Pressure Distributions on a 12' Span Wing of NACA 66-Series Airfoil Sections Up to a Mach Number of 0.60

naca-tn-1696-chordwise-pressure-distributions-on-a-12-span-wing-of-naca-66-series-airfoil-sections-up-to-a-mach-number-of-0-60-1

17,005 Documents in our Technical Library

2727926 Total Downloads