Small-scale investigation at transonic speeds of the effects of thickening the inboard section of a 45 degrees sweptback wing of aspect ratio 4, taper ratio 0.3, and NACA 65A006 airfoil section

Spreemann, Kenneth P Alford, William J , Jr
naca-rm-l51f08a
August 09, 1951


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l51f08a.pdf