1 // SIS Twin Otter Iced aircraft Nonlinear model
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3 // read readme_020212.doc for information
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5 #include "uiuc_iced_nonlin.h"
7 void Calc_Iced_Forces()
12 double eta_ref_wing = 0.08; // eta of iced data used for curve fit
13 double eta_ref_tail = 0.20; //changed from 0.12 10-23-2002
15 //double delta_CL; // CL_clean - CL_iced;
16 //double delta_CD; // CD_clean - CD_iced;
17 //double delta_Cm; // CM_clean - CM_iced;
18 double delta_Cm_a; // (Cm_clean - Cm_iced) as a function of AoA;
19 double delta_Cm_de; // (Cm_clean - Cm_iced) as a function of de;
32 alpha = Alpha*RAD_TO_DEG;
33 de = elevator*RAD_TO_DEG;
37 delta_CL = (0.088449 + 0.004836*alpha - 0.0005459*alpha*alpha +
38 4.0859e-5*pow(alpha,3));
42 delta_CL = (-11.838 + 1.6861*alpha - 0.076707*alpha*alpha +
43 0.001142*pow(alpha,3));
45 KCL = -delta_CL/eta_ref_wing;
46 eta_wing = 0.5*(eta_wing_left + eta_wing_right);
47 delta_CL = eta_wing*KCL;
51 delta_CD = (-0.0089 + 0.001578*alpha - 0.00046253*pow(alpha,2) +
52 -4.7511e-5*pow(alpha,3) + 2.3384e-6*pow(alpha,4));
53 KCD = -delta_CD/eta_ref_wing;
54 delta_CD = eta_wing*KCD;
56 // pitching moment fit
57 delta_Cm_a = (-0.01892 - 0.0056476*alpha + 1.0205e-5*pow(alpha,2)
58 - 4.0692e-5*pow(alpha,3) + 1.7594e-6*pow(alpha,4));
60 delta_Cm_de = (-0.014928 - 0.0037783*alpha + 0.00039086*pow(de,2)
61 - 1.1304e-5*pow(de,3) - 1.8439e-6*pow(de,4));
63 delta_Cm = delta_Cm_a + delta_Cm_de;
64 KCm_alpha = delta_Cm_a/eta_ref_wing;
65 KCm_de = delta_Cm_de/eta_ref_tail;
66 delta_Cm = (0.75*eta_wing + 0.25*eta_tail)*KCm_alpha + (eta_tail)*KCm_de;
71 delta_Ch_a = (-0.0012862 - 0.00022705*alpha + 1.5911e-5*pow(alpha,2)
72 + 5.4536e-7*pow(alpha,3));
78 delta_Ch_e = -0.0011851 - 0.00049924*de;
79 delta_Ch = -(delta_Ch_a + delta_Ch_e);
80 KCh = -delta_Ch/eta_ref_tail;
81 delta_Ch = eta_tail*KCh;
84 CL_diff = (eta_wing_left - eta_wing_right)*KCL;
85 delta_Cl = CL_diff/8.; // 10-23-02 Previously 4
88 CD_diff = (eta_wing_left - eta_wing_right)*KCD;
89 delta_Cn = CD_diff/8.;
93 void add_ice_effects()
95 CD_clean = -1*CX*Cos_alpha*Cos_beta - CY*Sin_beta - CZ*Sin_alpha*Cos_beta;
96 CY_clean = -1*CX*Cos_alpha*Sin_beta + CY*Cos_beta - CZ*Sin_alpha*Sin_beta;
97 CL_clean = CX*Sin_alpha - CZ*Cos_alpha;
103 CD_iced = CD_clean + delta_CD;
105 CL_iced = CL_clean + delta_CL;
106 Cm_iced = Cm_clean + delta_Cm;
107 Cl_iced = Cl_clean + delta_Cl;
108 Cn_iced = Cn_clean + delta_Cn;
109 //Ch_iced = Ch_clean + delta_Ch;
119 CX = -1*CD*Cos_alpha*Cos_beta - CY*Cos_alpha*Sin_beta + CL*Sin_alpha;
120 CY = -1*CD*Sin_beta + CY*Cos_beta;
121 CZ = -1*CD*Sin_alpha*Cos_beta - CY*Sin_alpha*Sin_beta - CL*Cos_alpha;