Читать книгу Flight Theory and Aerodynamics - Joseph R. Badick - Страница 72
EXAMPLE
ОглавлениеUsing the TAS from the previous example (518.6 kts.), when a = 607.3 kts., calculate the Mach number for the aircraft.
Using the TAS from the previous example (518.6 kts.), when a = 607.3 kts., calculate the Mach number for the aircraft.
