diff --git a/A319-100-CFM.xml b/A319-100-CFM.xml index 4e70c01a..2a887500 100644 --- a/A319-100-CFM.xml +++ b/A319-100-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A319-100-IAE.xml b/A319-100-IAE.xml index 80707b55..8e54cc0c 100644 --- a/A319-100-IAE.xml +++ b/A319-100-IAE.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A320-200-CFM.xml b/A320-200-CFM.xml index a24fc369..a84a9ba0 100644 --- a/A320-200-CFM.xml +++ b/A320-200-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A320-200-IAE.xml b/A320-200-IAE.xml index ab20ec08..371cd4d0 100644 --- a/A320-200-IAE.xml +++ b/A320-200-IAE.xml @@ -580,390 +580,21 @@ YAW MOI_________3950000______23089847_______24848934 + + - - - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A321-200-CFM.xml b/A321-200-CFM.xml index d8dbab47..324e2a2d 100644 --- a/A321-200-CFM.xml +++ b/A321-200-CFM.xml @@ -581,389 +581,20 @@ YAW MOI_________3950000______23089847_______24848934 - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/A321-200-IAE.xml b/A321-200-IAE.xml index d72b47ee..3b84756d 100644 --- a/A321-200-IAE.xml +++ b/A321-200-IAE.xml @@ -579,391 +579,22 @@ YAW MOI_________3950000______23089847_______24848934 - + - + - - - - Lift due to alpha - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -0.20 -0.900 - 0.00 0.103 - 0.15 1.600 - 0.23 1.900 - 0.60 1.000 - -
- - - - - Delta Lift due to flaps - - aero/qbar-psf - metrics/Sw-sqft - - fcs/flap-pos-norm - - 0.000 0.00000 - 0.290 0.00250 - 0.596 0.00700 - 0.645 0.01300 - 1.000 0.01700 - -
- - - - - Delta Lift due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/slat-pos-deg - 0.01000 - - - - - Delta Lift due to speedbrake - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - -0.15 - - - - - Lift due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-rad - 0.04 - - - - - - - - - Drag at zero lift - - aero/qbar-psf - metrics/Sw-sqft - - aero/alpha-rad - - -1.57 1.260 - -0.26 0.018 - 0.00 0.008 - 0.26 0.017 - 1.57 1.320 - -
- - - - - Induced drag - - aero/qbar-psf - metrics/Sw-sqft - aero/cl-squared - 0.035 - - - - - Drag due to mach - - aero/qbar-psf - metrics/Sw-sqft - - velocities/mach - - 0.00 0.000 - 0.79 0.000 - 1.10 0.023 - 1.80 0.015 - -
- - - - - Drag due to flaps - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00090 - - - - - Drag due to slats - - aero/qbar-psf - metrics/Sw-sqft - fcs/flap-pos-deg - 0.00120 - - - - - Drag due to gear - - aero/qbar-psf - metrics/Sw-sqft - gear/gear-pos-norm - 0.025 - - - - - Drag due to speedbrakes - - aero/qbar-psf - metrics/Sw-sqft - fcs/speedbrake-pos-norm - 0.035 - - - - - Drag due to sideslip - - aero/qbar-psf - metrics/Sw-sqft - - aero/beta-rad - - -1.57 1.230 - -0.26 0.050 - 0.00 0.000 - 0.26 0.050 - 1.57 1.230 - -
- - - - - Drag due to Elevator Deflection - - aero/qbar-psf - metrics/Sw-sqft - fcs/elevator-pos-norm - 0.035 - - - - - - - - - Side force due to beta - - aero/qbar-psf - metrics/Sw-sqft - aero/beta-rad - -1 - - - - - - - - - Roll moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - -0.1 - - - - - Roll moment due to roll rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/p-aero-rad_sec - -0.95 - - - - - Roll moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - 0.005 - - - - - Roll moment due to aileron - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0.20 - - - - - Roll moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - 0.003 - - - - - - - - - Pitch moment due to alpha - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/alpha-rad - -0.6 - - - - - Pitch moment due to elevator - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - fcs/elevator-pos-rad - - velocities/mach - - 0.0 -1.900 - 2.0 -0.900 - -
- - - - - Pitch moment due to pitch rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - velocities/q-aero-rad_sec - -140 - - - - - Pitch moment due to alpha rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/cbarw-ft - aero/ci2vel - aero/alphadot-rad_sec - -1 - - - - - - - - - Yaw moment due to beta - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/beta-rad - 0.12 - - - - - Yaw moment due to yaw rate - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - aero/bi2vel - velocities/r-aero-rad_sec - -0.2 - - - - - Yaw moment due to rudder - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/rudder-pos-rad - -0.2 - - - - - Adverse yaw - - aero/qbar-psf - metrics/Sw-sqft - metrics/bw-ft - fcs/left-aileron-pos-rad - 0 - - - - - - - - - - - 294 - 0 - -149 - - - 1 - 0 - 0 - - - + + + + 294 + 0 + -149 + + + 1 + 0 + 0 + + + diff --git a/Systems/a319-aerodynamics.xml b/Systems/a319-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a319-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + Drag due to sideslip + + aero/qbar-psf + metrics/Sw-sqft + + aero/beta-rad + + -1.57 1.230 + -0.26 0.050 + 0.00 0.000 + 0.26 0.050 + 1.57 1.230 + +
+ + + + + Drag due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-norm + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/a320-aerodynamics.xml b/Systems/a320-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a320-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + Drag due to sideslip + + aero/qbar-psf + metrics/Sw-sqft + + aero/beta-rad + + -1.57 1.230 + -0.26 0.050 + 0.00 0.000 + 0.26 0.050 + 1.57 1.230 + +
+ + + + + Drag due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-norm + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/a321-aerodynamics.xml b/Systems/a321-aerodynamics.xml new file mode 100644 index 00000000..318d7b8a --- /dev/null +++ b/Systems/a321-aerodynamics.xml @@ -0,0 +1,371 @@ + + + + + + + + Lift due to alpha + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -0.20 -0.900 + 0.00 0.103 + 0.15 1.600 + 0.23 1.900 + 0.60 1.000 + +
+ + + + + Delta Lift due to flaps + + aero/qbar-psf + metrics/Sw-sqft + + fcs/flap-pos-norm + + 0.000 0.00000 + 0.290 0.00250 + 0.596 0.00700 + 0.645 0.01300 + 1.000 0.01700 + +
+ + + + + Delta Lift due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/slat-pos-deg + 0.01000 + + + + + Delta Lift due to speedbrake + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + -0.15 + + + + + Lift due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-rad + 0.04 + + + + + + + + + Drag at zero lift + + aero/qbar-psf + metrics/Sw-sqft + + aero/alpha-rad + + -1.57 1.260 + -0.26 0.018 + 0.00 0.008 + 0.26 0.017 + 1.57 1.320 + +
+ + + + + Induced drag + + aero/qbar-psf + metrics/Sw-sqft + aero/cl-squared + 0.035 + + + + + Drag due to mach + + aero/qbar-psf + metrics/Sw-sqft + + velocities/mach + + 0.00 0.000 + 0.79 0.000 + 1.10 0.023 + 1.80 0.015 + +
+ + + + + Drag due to flaps + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to slats + + aero/qbar-psf + metrics/Sw-sqft + fcs/flap-pos-deg + 0.00080 + + + + + Drag due to gear + + aero/qbar-psf + metrics/Sw-sqft + gear/gear-pos-norm + 0.025 + + + + + Drag due to speedbrakes + + aero/qbar-psf + metrics/Sw-sqft + fcs/speedbrake-pos-norm + 0.035 + + + + + Drag due to sideslip + + aero/qbar-psf + metrics/Sw-sqft + + aero/beta-rad + + -1.57 1.230 + -0.26 0.050 + 0.00 0.000 + 0.26 0.050 + 1.57 1.230 + +
+ + + + + Drag due to Elevator Deflection + + aero/qbar-psf + metrics/Sw-sqft + fcs/elevator-pos-norm + 0.035 + + + + + + + + + Side force due to beta + + aero/qbar-psf + metrics/Sw-sqft + aero/beta-rad + -1 + + + + + + + + + Roll moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + -0.1 + + + + + Roll moment due to roll rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/p-aero-rad_sec + -0.95 + + + + + Roll moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + 0.005 + + + + + Roll moment due to aileron + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0.20 + + + + + Roll moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + 0.003 + + + + + + + + + Pitch moment due to alpha + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/alpha-rad + -0.6 + + + + + Pitch moment due to elevator + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + fcs/elevator-pos-rad + + velocities/mach + + 0.0 -1.900 + 2.0 -0.900 + +
+ + + + + Pitch moment due to pitch rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + velocities/q-aero-rad_sec + -140 + + + + + Pitch moment due to alpha rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/cbarw-ft + aero/ci2vel + aero/alphadot-rad_sec + -1 + + + + + + + + + Yaw moment due to beta + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/beta-rad + 0.12 + + + + + Yaw moment due to yaw rate + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + aero/bi2vel + velocities/r-aero-rad_sec + -0.2 + + + + + Yaw moment due to rudder + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/rudder-pos-rad + -0.2 + + + + + Adverse yaw + + aero/qbar-psf + metrics/Sw-sqft + metrics/bw-ft + fcs/left-aileron-pos-rad + 0 + + + + + diff --git a/Systems/fadec-cfm.xml b/Systems/fadec-cfm.xml index 5057b01d..add9e078 100644 --- a/Systems/fadec-cfm.xml +++ b/Systems/fadec-cfm.xml @@ -1,5 +1,8 @@ + + + @@ -436,7 +439,7 @@ /engines/engine[0]/n1 - 23 + 22 @@ -469,7 +472,7 @@ /engines/engine[1]/n1 - 23 + 22 diff --git a/Systems/fadec-iae.xml b/Systems/fadec-iae.xml index 1a72e389..c0d91476 100644 --- a/Systems/fadec-iae.xml +++ b/Systems/fadec-iae.xml @@ -1,5 +1,8 @@ + + + @@ -702,7 +705,7 @@ /engines/engine[0]/n1 - 23 + 22 @@ -735,7 +738,7 @@ /engines/engine[1]/n1 - 23 + 22 @@ -755,4 +758,4 @@ /engines/engine[1]/egt-actual - + \ No newline at end of file