Choose the correct statement:
Mach number = True Air Speed (TAS) / Local Speed of Sound (LSS)
LSS = 38.96 √ Absolute Temperature (K)
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IAS = 1/2 p V2 (Where V = TAS)
When flying into a colder airmass, density "p" increases. In order to maintain IAS constant, TAS (V) must decrease. -
LSS will decrease in colder air.
As both TAS and LSS decreases, Mach number will not change.
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