abridged list of the specifications provided to us by L-3. The main applications of interest we are comparing our data to are Aeromatic and Datacom. AeroMatic Input AeroMatic Output AeroMatic Input AeroMatic Output # engines speedbrake control [engine config] empty weight engine type engine type CG location (x,y,z) engine layout CL (alpha) horsepower,# ? (X,Y,Z) (CENTER yaw damper OF PRESSURE?) afterburning pilot eye location CL(elevator deflection) (x,y,z) water injection landing gear nose specs dCL(flap) left landing gear specs AeroMatic Output dCL(speedbrake) right landing gear [propeller config] specs engine power, # engine location generated in file Zero lift drag (x,y,z,pitch, yaw, feed) (..._engine.xml) rpm, # thrust location milthrust Induced Drag (x,y,z,pitch,yaw) pitch fuel tank0 size and max thrust CD(mach) location (x,y,z,radius, capacity, contents) propeller dia, # fuel tank1 size and bypass ratio CD(flap) location (x,y,z,radius, capacity, contents) pitch trim idleN1 CD(gear) [aero config] elevator control MAXN1 CD(speedbrakes) aircraft type roll trim MAXN2 CD(Sideslip) TO weight, # left aileron control thrust coeff CD(elevator deflection) wingspan, # right aileron control idle power thrust factor vs. vel and postion plane length,# rudder command military power thrust Cy(beta) factor vs. vel and AeroMatic Input AeroMatic Output AeroMatic Input AeroMatic Output wing area,# rudder control c_thrust (table) Cm(elevator) landing gear flaps control c_power (table) Cm(pitch rate) retractable gear control generated in file Cm(a dot) (..._aero.xml) roll moment, Cl, due to horizontal tail area beta generated in file Cl(roll rate) horizontal tail arm Yaw moment, Cn, due (..._prop.xml) to beta linear blade inches Cl(yaw rate) vertical tail area Cn(yaw rate) Ixx Cl(aileron) Ixx min pitch Cl(rudder) Iyy
abridged list of the specifications provided to us by L-3. The main applications of interest we are comparing our data to are Aeromatic and Datacom. AeroMatic Input AeroMatic Output AeroMatic Input AeroMatic Output # engines speedbrake control [engine config] empty weight engine type engine type CG location (x,y,z) engine layout CL (alpha) horsepower,# ? (X,Y,Z) (CENTER OF PRESSURE?) yaw damper afterburning pilot eye location (x,y,z) CL(elevator deflection) water injection landing gear nose specs dCL(flap) left landing gear specs AeroMatic Output dCL(speedbrake) [propeller config] right landing gear specs engine power, # engine location (x,y,z,pitch, yaw, feed) generated in file (..._engine.xml) Zero lift drag rpm, # thrust location (x,y,z,pitch,yaw) milthrust Induced Drag pitch fuel tank0 size and location (x,y,z,radius, capacity, contents) max thrust CD(mach) propeller dia, # fuel tank1 size and location (x,y,z,radius, capacity, contents) bypass ratio CD(flap) pitch trim idleN1 CD(gear) [aero config] elevator control MAXN1 CD(speedbrakes) aircraft type roll trim MAXN2 CD(Sideslip) TO weight, # left aileron control thrust coeff CD(elevator deflection) wingspan, # right aileron control idle power thrust factor vs. vel and postion plane length,# rudder command military power thrust factor vs. vel and Cy(beta) AeroMatic Input AeroMatic Output AeroMatic Input AeroMatic Output wing area,# rudder control c_thrust (table) Cm(elevator) landing gear flaps control c_power (table) Cm(pitch rate) retractable gear control generated in file (..._aero.xml) Cm(a dot) roll moment, Cl, due to beta horizontal tail area generated in file (..._prop.xml) Cl(roll rate) horizontal tail arm Yaw moment, Cn, due to beta linear blade inches Cl(yaw rate) vertical tail area Cn(yaw rate) Ixx Cl(aileron) Ixx min pitch Cl(rudder) Iyy
FDL%20SD2%20Paper.docx