MATLAB The Mach number is a critical quantity in aerodynamics. It is the ratio of the speed of an object (e.g., an aircraft) to the speed of sound. If the Mach number is less than 1, the flow is subsonic; if the Mach number is between (0.8-1.2), the flow is transonic; if the Mach number is equal to 1, the flow is sonic; if the Mach number is between (1.2 and 5), the flow is supersonic; if the Mach number is greater than 5, the flow is hypersonic. Write a script that will prompt the user for the speed of an aircraft and the speed of sound at the aircraft's current altitude and will print whether the condition is subsonic, transonic, sonic, supersonic or hypersonic.
MATLAB The Mach number is a critical quantity in aerodynamics. It is the ratio of the speed of an object (e.g., an aircraft) to the speed of sound. If the Mach number is less than 1, the flow is subsonic; if the Mach number is between (0.8-1.2), the flow is transonic; if the Mach number is equal to 1, the flow is sonic; if the Mach number is between (1.2 and 5), the flow is supersonic; if the Mach number is greater than 5, the flow is hypersonic. Write a script that will prompt the user for the speed of an aircraft and the speed of sound at the aircraft's current altitude and will print whether the condition is subsonic, transonic, sonic, supersonic or hypersonic.
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Transcribed Image Text:MATLAB
The Mach number is a critical quantity
in aerodynamics. It is the ratio of the
speed of an object (e.g., an aircraft) to
the speed of sound. If the Mach
number is less than 1, the flow is
subsonic; if the Mach number is
between (0.8-1.2), the flow is
transonic; if the Mach number is equal
to 1, the flow is sonic; if the Mach
number is between (1.2 and 5), the flow
is supersonic; if the Mach number is
greater than 5, the flow is hypersonic.
Write a script that will prompt the user
for the speed of an aircraft and the
speed of sound at the aircraft's current
altitude and will print whether the
condition is subsonic, transonic, sonic,
supersonic or hypersonic.
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