An Experimental Investigation of the Effects of Canard Position on the Aerodynamic Forces of a Fighter Type Configuration Model

M. Manshadi; A. Sharafi; M.H. Soltani

Volume 9, Issue 2 , September 2012, , Pages 15-24

Abstract
  An extensive experimental investigation is conducted to study the effect of canard position relative to the fuselage reference line on the aerodynamic forces of a fighter type configuration model. Aerodynamic forces at different flight conditions are measured in a subsonic wind tunnel. The wing and the ...  Read More

Effects of Pitching Motion on Shock Behavior in a Body-Wrap Around Fin Configuration

hamid fazeli; M.R. Soltani; alireza davari

Volume 7, Issue 1 , March 2010, , Pages 51-57

Abstract
  Unsteady dynamic behavior of TTCP model with different wrap around fin sets were investigated in a trisonic wind tunne. The aerodynamic coefficient force measurement in this wind tunnel shows good agreement in comparison with that of the NASA Langley Research Center in static case. The model was sinusoidally ...  Read More