An investigation at transonic speeds of the effects of control chord and span on the control characteristics of a tapered wedge-type wing of aspect ratio 2.5 : transonic-bump method

Vogler, Raymond D Turner, Thomas R Lockwood, Vernard, E
naca-rm-l51g03
September 20, 1951


No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1951/naca-rm-l51g03.pdf