%---------------------------------------------------------------------------
% Model Reference Data (one record per polar)		 / NG / 11-Feb-2014
$$CONSDAT
% ~~~~~~~
Config				! Configuration number	 [349101,...]
Assembly			! Model assembly	 [B+W+BF+N+P,...]
HTP				! Horiz. tail plane	 [On,Off]
Fixing				! Transition fixing	 [On,Off]
Markers				! SPT markers		 [On]
Coating				! PIV coating		 [On]
%
% Wing Pressure Taps - X Locations (trailing edge -> leading edge -> TE)
X_A(1:32)			! Wing Section 1, Eta=0.131
X_B(1:31)			! Wing Section 2, Eta=0.201
X_C(1:33)			! Wing Section 3, Eta=0.283
X_D(1:18)			! Wing Section 4, Eta=0.397
X_DP(1:9)			!   "     "    4, port
X_E(1:22)			! Wing Section 5, Eta=0.502
X_EP(1:9)			!   "     "    5, port
X_F(1:20)			! Wing Section 6, Eta=0.603
X_G(1:25)			! Wing Section 7, Eta=0.727
X_GP(1:8)			!   "     "    7, port
X_H(1:24)			! Wing Section 8, Eta=0.846
X_I(1:22)			! Wing Section 9, Eta=0.950
%
% Spanwise Positions for Bending and Twist Evaluation [m]
WSpans(1:11)			! Wing
HSpans(1:11)			! HTP
%
$$Y_CRDMP
% ~~~~~~~
% Wing Pressure Taps - Y Locations
Y_A(1:32), Y_B(1:31), Y_C(1:33)
Y_D(1:18), Y_DP(1:9)
Y_E(1:22), Y_EP(1:9)
Y_F(1:20)
Y_G(1:25), Y_GP(1:8)
Y_H(1:24), Y_I(1:22)
%
%---------------------------------------------------------------------------
% Test Results Data according to Customer Requirements	 / NG / 24-Feb-2014
$$CUSDAT
% ~~~~~~
% Identification Data
SerNo				! Series number
PolNo				! Polar number
DPNo				! Datapoint number
%
% Reference Dimensions
S_ref				! Reference area (temperature dependent) [m²]
AMC				! Aerodynamic mean chord (temp. dependent) [m]
%
% Flow Reference Conditions
M				! Reference Mach number
Re				! Reynolds Number for reference length
Pt				! Tunnel total pressure [Pa]
Ps				! Tunnel static pressure [Pa]
P_Plenum			! Plenum pressure [Pa]
Q				! Free-stream dynamic pressure [Pa]
QoE				! Normalized dynamic pressure *1e6
Tt				! Tunnel total temperature [K]
Ts				! Tunnel static temperature [K]
%
% Model Attitude
Alpha				! AoA (fully corrected, inclinometer based) [°]
Beta				! Sideslip angle [°]
Phi				! Model roll angle [°]
%
% Aerodynamic Coefficients (Body and Air-path Axes Systems)
% Body Axes System 
CA				! Axial force coefficient
CYA				! Lateral force coeficient
CN				! Normal force coefficient
CLA				! Rolling  moment coefficient
CMA25				! Pitching    "	      "
CNA				! Yawing      "	      "
%
% Air-path Axes System
CD, CY, CL			! Drag, lateral force, lift coefficient
CDV				! CD-CL²/Pi/Lambda
CRoll				! Rolling  moment coefficient
CM				! Pitching    "       "
CYaw				! Yawing      "       "
%
% Wing Root Buffet Gauge
WrBG				! Filtered signal [V]
WrBG_rms			! RMS value [V]
%
% Model Temperatures [K]
TM1_Nose			! Model nose
TM2_FusF			! Fuselage front
TM3_FusR			! Fuselage rear
%
% Wing Pressure Coefficients (trailing edge -> leading edge -> TE)
Cp_A(1:32)			! Wing Section 1, Eta=0.131
Cp_B(1:31)			! Wing Section 2, Eta=0.201
Cp_C(1:33)			! Wing Section 3, Eta=0.283
Cp_D(1:18)			! Wing Section 4, Eta=0.397
Cp_DP(1:9)			!   "     "    4, port
Cp_E(1:22)			! Wing Section 5, Eta=0.502
Cp_EP(1:9)			!   "     "    5, port
Cp_F(1:20)			! Wing Section 6, Eta=0.603
Cp_G(1:25)			! Wing Section 7, Eta=0.727
Cp_GP(1:8)			!   "     "    7, port
Cp_H(1:24)			! Wing Section 8, Eta=0.846
Cp_I(1:22)			! Wing Section 9, Eta=0.950
%
% Sting Cavity Pressure Coefficients
Cp_StCav1			! Starboard, upstream
Cp_StCav2			! Starboard
Cp_StCav3			! Starboard
Cp_StCav4			! Port, upstream
Cp_StCav5			! Port
Cp_StCav6			! Port
%
% Wing Bending [mm] and Twist [°]
VInpGPR(101)=WBend(1)		! Y=.0873, Eta=0.11  (wing root)
VInpGPR(102)=WBend(2)		! Y=.1587, Eta=0.2
VInpGPR(103)=WBend(3)		! Y=.2380, Eta=0.3
VInpGPR(104)=WBend(4)		! Y=.3173, Eta=0.4
VInpGPR(105)=WBend(5)		! Y=.3967, Eta=0.5
VInpGPR(106)=WBend(6)		! Y=.4760, Eta=0.6
VInpGPR(107)=WBend(7)		! Y=.5553, Eta=0.7
VInpGPR(108)=WBend(8)		! Y=.6346, Eta=0.8
VInpGPR(109)=WBend(9)		! Y=.7140, Eta=0.9
VInpGPR(110)=WBend(10)		! Y=.7536, Eta=0.95
VInpGPR(111)=WBend(11)		! Y=.7933, Eta=1.00
Twists(1:11)=WTwist(1:11)
%
% HTP Bending [mm] and Twist [°]
VInpGPR(121)=HBend(1)		! Y=.0461, Eta=0.16  (HTP root)
VInpGPR(122)=HBend(2)		! Y=.0576, Eta=0.2
VInpGPR(123)=HBend(3)		! Y=.0864, Eta=0.3
VInpGPR(124)=HBend(4)		! Y=.1152, Eta=0.4
VInpGPR(125)=HBend(5)		! Y=.1440, Eta=0.5
VInpGPR(126)=HBend(6)		! Y=.1728, Eta=0.6
VInpGPR(127)=HBend(7)		! Y=.2016, Eta=0.7
VInpGPR(128)=HBend(8)		! Y=.2304, Eta=0.8
VInpGPR(129)=HBend(9)		! Y=.2592, Eta=0.9
VInpGPR(120)=HBend(10)		! Y=.2736, Eta=0.95
VInpGPR(121)=HBend(11)		! Y=.2880, Eta=1.00
Twists1(1:11)=HTwist(1:11)
%
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