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@ -17,7 +17,7 @@ Speed conversion at altitude H[m] in ISA
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Mach = tas2mach(Vtas,H) # true airspeed (Vtas) to mach number conversion
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Mach = tas2mach(Vtas,H) # true airspeed (Vtas) to mach number conversion
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Vtas = mach2tas(Mach,H) # true airspeed (Vtas) to mach number conversion
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Vtas = mach2tas(Mach,H) # mach number to true airspeed (Vtas) conversion
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Vtas = eas2tas(Veas,H) # equivalent airspeed to true airspeed, H in [m]
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Vtas = eas2tas(Veas,H) # equivalent airspeed to true airspeed, H in [m]
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Veas = tas2eas(Vtas,H) # true airspeed to equivent airspeed, H in [m]
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Veas = tas2eas(Vtas,H) # true airspeed to equivent airspeed, H in [m]
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Vtas = cas2tas(Vcas,H) # Vcas to Vtas conversion both m/s, H in [m]
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Vtas = cas2tas(Vcas,H) # Vcas to Vtas conversion both m/s, H in [m]
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