An experimental investigation of the zero-lift-drag characteristics of symmetrical blunt-trailing-edge airfoils at Mach numbers from 2.7 to 5.0

Syvertson, Clarence A Gloria, Hermilo R
naca-rm-a53b02
April 29, 1953


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1953/naca-rm-a53b02.pdf