Aircraft FM changes: (by prae) (reminder that this is not the latest version, there will be more FM changes after this)
Eurofighter [DEU], F-2000A, Typhoon F.G.R. Mk. 4:
flap control enabled, now has takeoff flaps (90% deployment) and landing flaps (100% deployment)
wing adjustments:
gear wing arm shift changed from [0.05, 0.0] to [0.01, 0.1]
0% flap deployment:
Oswald’s efficiency number decreased from 0.53 to 0.5
zero-lift drag Mach multiplier curve multiplier max decreased from 1.65 to 1.55
zero-lift drag coefficient will now peak lower at M1.07, allowing for higher top speeds (Comparison)
新的
[23:52]
100% flap deployment:
Oswald’s efficiency number decreased from 0.53 to 0.44
coefficient of lift after high critical angle decreased from 1.7 to 1.6
coefficient of lift after low critical angle decreased from -0.8 to -1.4
zero-lift drag Mach multiplier curve multiplier max increased from 1.65 to 1.95
zero-lift drag coefficient will now peak higher at M1.07, but will be decreased in general due to lower CdMin (Comparison)
indcued drag multiplier Mach multiplier curve multiplier max increased from 0.78 to 0.81
induced drag multiplier will now peak lower at M0.6, but still be increased in general due to lower Oswald’s efficiency number (Comparison)
zero-drag lift coefficient decreased from 0.35 to 0.25
coefficient of lift at critical angle decreased from -0.8 to -1.2
zero-lift drag coefficient decreased from 0.018 to 0.014
VNE (rip speed) increased from 1543 km/h IAS to 1607 km/h IAS
MNE (rip speed by mach) increased from M2.0 to M2.46
fuselage adjustments:
zero-lift drag Mach multiplier curve multiplier max decreased from 2.45 to 2.1
zero-lift drag coefficient will now peak lower at M1.16, allowing for higher top speeds (Comparison)
zero-lift drag coefficient decreased from 0.008 to 0.007
thrust adjustments:
at sea level
general decrease in afterburning thrust ranging from 2000-5000 kgf (Comparison)
general decrease in military power (100%) thrust ranging from 300-600 kgf at 200-2000 km/h TAS (Comparison)
新的
[23:52]
empty mass increased from 11500 kg to 11700 kg
新的
[23:53]
Rafale C (F3R):
wing, 100% flaps deployment zero-lift drag coefficient increased from 0.007 to 0.011
fuselage zero-lift drag coefficient Mach multiplier curve adjustments
Mach number of coefficient max from 1.16 to 1.19
Mach multiplier max from 2.65 to 2.2
now the fuselage’s zero-lift drag coefficient will now peak at M1.19 instead of M1.16 and lower than before (Comparison)
horizontal stabilizer zero-lift drag coefficient Mach multiplier curve Mach number of coefficient max from 0.97 to 1.1
now the horizontal stabilizer’s zero-lift drag coefficient will peak at M1.1 instead of M0.97 (Comparison)
thrust adjustments:
at 3000 m: decrease in afterburning thrust of about 400 kgf from 1600-2000 km/h TAS (Comparison)
at 6000 m: decrease in afterburning thrust of about 400-500 kgf from 1600-2000 km/h TAS (Comparison)
at 9000 m: decrease in afterburning thrust of about 200-500 kgf from 1400-2000 km/h TAS (Comparison)
at 12000 m: decrease in afterburning thrust of about 80-400 kgf from 1200-2000 km/h TAS (Comparison)
at 15000 m: decrease in afterburning thrust of about 100-200 kgf from 1200-2000 km/h TAS (Comparison)
empty mass decreased from 10300 kg to 9700 kg
max fuel mass increased from 9160 kg to 9560 kg
看不懂 大概是台风阵风包线图有变化