.:instrumentfiles:CitationWinds

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1)  Air_Temp_w: Air Temperature Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius]
2)    MachNo_w: Mach Number based on Wing Pitot Pressure
3)       IAS_w: Indicated Air Speed based on Wing Pitot Pressure [m/s]
4)       TAS_w: True Air Speed based on Wing Pitot Pressure [m/s] {Calibration:  slope = 60.797701 offset = -150.48263}
5)   Press_Alt: Pressure Altitude [m]
6)  Alpha_nose: Alpha (Attack) Angle based on Nose Pitot Pressure [degrees] {Calibration:  slope = 0.078381400 offset = 0.66263812}
7)   Beta_nose: Beta (Sideslip) Angle based on Nose Pitot Pressure [degrees] {Calibration:  slope = 0.082174510 offset = 0.048555200}
8)        GS_X: X (East) Component of the Ground Speed [m/s]
9)        GS_Y: Y (North) Component of the Ground Speed [m/s]

10) VERT_VEL: Vertical Velocity of the aircraft based on the change in position over a 2 seceond interval [m/s] 11) Wind_X_Nose: X (East) Component of the Wind Speed based on the Nose Probe [m/s] 12) Wind_Y_Nose: Y (North) Component of the Wind Speed based on the Nose Probe [m/s] 13) Wind_Z_Nose: Z (Vertical) Component of the Wind Speed based on the Nose Probe (postive value is upward, away from the Earth's surface) [m/s] 14) Wind_M_Nose: Horizontal Wind Speed based on the Nose Probe [m/s] 15) Wind_D_Nose: Horizontal Wind Direction from Nose Probe [degrees]; True Direction From Which it Blows 16) Wind_X_Wing: X (East) Component of the Wind Speed based on the Wing Probe [m/s] 17) Wind_Y_Wing: Y (North) Component of the Wind Speed based on the Wing Probe [m/s] 18) Wind_Z_Wing: Z (Vertical) Component of the Wind Speed based on the Wing Probe (positive value is upward, away from the Earth's surface) [m/s] 19) Wind_M_Wing: Horizontal Wind Speed based on the Wing Probe [m/s] 20) Wind_D_Wing: Horizontal Wind Direction from Wing Probe [degrees]; True Direction From Which it Blows 21) Wind_X: X (East) Component of the Wind Speed [m/s] 22) Wind_Y: Y (North) Component of the Wind Speed [m/s] 23) Wind_Z: Z (Vertical) Component of the Wind Speed (postivie value is upward, away from the Earth's surface) [m/s] 24) Wind_M: Horizontal Wind Speed [m/s] 25) Wind_D: Horizontal Wind Direction [degrees]; True Direction From Which it Blows 26) TURB: Turbulence parameter (Eddy Dissipation Rate) based on Wing Pitot pressure [cm^2/3*s^-1] 27) PFlag: Wind Parameter Flag 28) Air_Temp_n: Air Temperature Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] 29) MachNo_n: Mach Number based on Nose Pitot Pressure 30) IAS_n: Indicated Air Speed based on Nose Pitot Pressure [m/s] 31) TAS_n: True Air Speed based on Nose Pitot Pressure [m/s] {Calibration: slope = 16.033642 offset = 2.2182522} 32) TURB_n: Turbulence parameter (Eddy Dissipation Rate) based on Nose Pitot pressure [cm^2/3*s^-1] 33) Pot_Temp: Potential Temperature [K] 34) Air_Temp2_w: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Wing Pitot Pressure [degrees Celsius] 35) Air_Temp2_n: Air Temperature from Rosemount Left Wing (#2) Probe Corrected for Dynamic Heating based on Nose Pitot Pressure [degrees Celsius] 36) TAS: True Air Speed based first on the Pitot Nose Pressure measurements (if available) and then on the Wing Pitot Pressure measurement [m/s] 37) Air_Temp: Air Temperature Corrected for Dynamic Heating based first on the Pitot Nose Pressure measurement (if available) and then based on the Pitot Wing Pressure measurement [degrees Celsius] 38) TAS_Flag: True Air Speed Flag (Ones place indicates if Pitot Nose or Pitot Wing is used, Tens place indicates if Temperature Probe #1 or #2 is used) 39) TAS_X_nose: X (East) Component of the True Air Speed based on Nose Probe [m/s] 40) TAS_Y_nose: Y (North) Component of the True Air Speed based on Nose Probe[m/s] 41) Alpha_wing: Alpha (Attack) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} 42) Beta_wing: Beta (Sideslip) Angle based on Wing Pitot Pressure [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200} 43) Alpha: Alpha (Attack) Angle [degrees] {Calibration: slope = 0.078381400 offset = 0.66263812} 44) Beta: Beta (Sideslip) Angle [degrees] {Calibration: slope = 0.082174510 offset = 0.048555200}