Je suis tombé là dessus, quelqu'un pour confirmer mon interprétation ?
CITATION
SFM_engine_table = {}
SFM_engine_table[Su_27] = {
typeng = 1,
dcx_eng = 0.0124,
hMaxEng = 19.5,
dpdh_f = 14500.,
dpdh_m = 7000.,
engtab1 = {
-- M Pmax Pfor
0.0, 135000., 205000.,
0.2, 124000., 175000.,
0.4, 114000., 171000.,
0.6, 110800., 180000.,
0.7, 109900., 192000.,
0.8, 109900., 210000.,
0.9, 109900., 228000.,
1.0, 110800., 240000.,
1.1, 113400., 256000.,
1.2, 119400., 265000.,
1.3, 134100., 279000.,
1.5, 155000., 300000.,
1.8, 165000., 331000.,
2.0, 165000., 356000.,
2.2, 165000., 375000.,
2.5, 165000., 386000.,
3.9, 165000., 270476.
}
}
SFM_engine_table[Su_27] = {
typeng = 1,
dcx_eng = 0.0124,
hMaxEng = 19.5,
dpdh_f = 14500.,
dpdh_m = 7000.,
engtab1 = {
-- M Pmax Pfor
0.0, 135000., 205000.,
0.2, 124000., 175000.,
0.4, 114000., 171000.,
0.6, 110800., 180000.,
0.7, 109900., 192000.,
0.8, 109900., 210000.,
0.9, 109900., 228000.,
1.0, 110800., 240000.,
1.1, 113400., 256000.,
1.2, 119400., 265000.,
1.3, 134100., 279000.,
1.5, 155000., 300000.,
1.8, 165000., 331000.,
2.0, 165000., 356000.,
2.2, 165000., 375000.,
2.5, 165000., 386000.,
3.9, 165000., 270476.
}
}
Il me semble que c'est lié à la poussée fournie en fonction du mach, ou un truc de ce style. Si ça évoque quelquechose à nos chers ingés aéros
Si c'est le cas, vu l'évolution des valeurs autour de mach 1, y'aurait un réel intérêt à s'éloigner le plus possible de mach 1, comme en vrai
Edit :
encore mieux ici, mais carrément besoin de traduction
CITATION
SFM_aerod_table[Su_27] = {
kjx = 2.7,
kjz = 0.00125,
Czbe = -0.016,
cx_gear = 0.0268,
cx_flap = 0.05,
cy_flap = 0.5,
cx_brk = 0.06,
aertab1 = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
0.0, 0.0165, 0.070, 0.1, 0.032, 0.5, 30., 1.6,
0.2, 0.0165, 0.070, 0.1, 0.032, 1.5, 30., 1.6,
0.4, 0.0165, 0.070, 0.1, 0.032, 2.5, 30., 1.6,
0.6, 0.0165, 0.073, 0.094, 0.043, 3.5, 30., 1.5,
0.7, 0.0170, 0.076, 0.094, 0.045, 3.5, 28.5, 1.45,
0.8, 0.0178, 0.079, 0.094, 0.048, 3.5, 27., 1.4,
0.9, 0.0215, 0.083, 0.11, 0.050, 3.5, 25.5, 1.3,
1.0, 0.0310, 0.085, 0.15, 0.1, 3.5, 24., 1.2,
1.1, 0.0422, 0.086, 0.15, 0.1, 3.15, 18., 1.1,
1.2, 0.0440, 0.083, 0.14, 0.1, 2.45, 17., 1.05,
1.3, 0.0432, 0.077, 0.17, 0.096, 1.75, 16., 1.0,
1.5, 0.0423, 0.062, 0.23, 0.09, 1.5, 13., 0.9,
1.8, 0.0416, 0.046, 0.23, 0.38, 0.9, 12., 0.7,
2.0, 0.0416, 0.039, 0.08, 2.5, 0.8, 10.5, 0.55,
2.2, 0.0416, 0.034, 0.16, 3.2, 0.7, 9., 0.4,
2.5, 0.0410, 0.033, 0.25, 4.5, 0.7, 9., 0.4,
3.9, 0.0395, 0.033, 0.35, 6., 0.7, 9., 0.4
}
}
kjx = 2.7,
kjz = 0.00125,
Czbe = -0.016,
cx_gear = 0.0268,
cx_flap = 0.05,
cy_flap = 0.5,
cx_brk = 0.06,
aertab1 = {
-- M Cx0 Cya B B4 Omxmax Aldop Cymax
0.0, 0.0165, 0.070, 0.1, 0.032, 0.5, 30., 1.6,
0.2, 0.0165, 0.070, 0.1, 0.032, 1.5, 30., 1.6,
0.4, 0.0165, 0.070, 0.1, 0.032, 2.5, 30., 1.6,
0.6, 0.0165, 0.073, 0.094, 0.043, 3.5, 30., 1.5,
0.7, 0.0170, 0.076, 0.094, 0.045, 3.5, 28.5, 1.45,
0.8, 0.0178, 0.079, 0.094, 0.048, 3.5, 27., 1.4,
0.9, 0.0215, 0.083, 0.11, 0.050, 3.5, 25.5, 1.3,
1.0, 0.0310, 0.085, 0.15, 0.1, 3.5, 24., 1.2,
1.1, 0.0422, 0.086, 0.15, 0.1, 3.15, 18., 1.1,
1.2, 0.0440, 0.083, 0.14, 0.1, 2.45, 17., 1.05,
1.3, 0.0432, 0.077, 0.17, 0.096, 1.75, 16., 1.0,
1.5, 0.0423, 0.062, 0.23, 0.09, 1.5, 13., 0.9,
1.8, 0.0416, 0.046, 0.23, 0.38, 0.9, 12., 0.7,
2.0, 0.0416, 0.039, 0.08, 2.5, 0.8, 10.5, 0.55,
2.2, 0.0416, 0.034, 0.16, 3.2, 0.7, 9., 0.4,
2.5, 0.0410, 0.033, 0.25, 4.5, 0.7, 9., 0.4,
3.9, 0.0395, 0.033, 0.35, 6., 0.7, 9., 0.4
}
}