ordinates-and-theoretical-pressure-distribution-data-for-naca-6--and-6a-series-airfoil-sections-with-thicknesses-from-2-to-21-and-from-2-to-15-percent-chord--respectively

Ordinates And Theoretical Pressure Distribution Data For NACA 6 And 6A Series Airfoil Sections With Thicknesses From 2 To 21 And From 2 To 15 Percent Chord Respectively

You must registered to download this book.
Sign Up to make free account below! now before expired!

Sign Up

Disclaimer : “contain affiliate links to Amazon.com. As an Amazon Associate, I earn from qualifying purchases”. Need Help? Contact us