Appendix 3: List of parameters Parameters USI US/Imp Fuselage Height: HEIGHTfus Width: WIDTHfus Length: LENGTHfus Wing span: b Aspect Ratio: AR Gross Surface: S Exposed: S_exp Taper Ratio: Lambda Cord at root: Croot Cord at tip: Ctip Sweep angle at chord quarter: Lambda_quart Geometric twist: Eps_gtip Mean Aerodynamic Chord: MAC X coordinate of Aerodynamic center: Xac Y coordinate of Aerodynamic center: Yac Compressibility parameter: BETA Cruise Mach: M Average airfoil thickness: t_bar Fuel volume: V_fuel Wetted wing surface: S_wetted_w Wing lift coefficient in cruise: C_L_w Wing lift coefficient derivative: a
Appendix 3: List of parameters Parameters USI US/Imp Fuselage Height: HEIGHTfus Width: WIDTHfus Length: LENGTHfus Wing span: b Aspect Ratio: AR Gross Surface: S Exposed: S_exp Taper Ratio: Lambda Cord at root: Croot Cord at tip: Ctip Sweep angle at chord quarter: Lambda_quart Geometric twist: Eps_gtip Mean Aerodynamic Chord: MAC X coordinate of Aerodynamic center: Xac Y coordinate of Aerodynamic center: Yac Compressibility parameter: BETA Cruise Mach: M Average airfoil thickness: t_bar Fuel volume: V_fuel Wetted wing surface: S_wetted_w Wing lift coefficient in cruise: C_L_w Wing lift coefficient derivative: a
EnonceConception_20172018_table.docx