.:instrumentfiles:CitationWinds

 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}