Investigation of effect of sideslip on lateral stability characteristics II : rectangular midwing on circular fuselage with variations in vertical-tail area and fuselage length with and without horizontal tail surface

Hollingworth, Thomas A
naca-wr-l-8
April 1945

No Abstract Available

An Adobe Acrobat (PDF) file of the entire report:
http://naca.central.cranfield.ac.uk/reports/1945/naca-wr-l-8.pdf