e Chegg Study | Guided S: \ e Chegg Study l Guided s x / D Assignment 4.pdf \ Secure https://app.lms unimelb.edu.au/bbcswebdav/pid-5834078-dt content-rid-242941412/courses/ENGR100032017 SM2/Assignment 4.pdf : Apps G Google - My Home-Blackbo Login-The Universi: Watch Game of Thro Assignment 4.pdf 4 17 In aerodynamics, the Mach number is a critical quantity. It is defined as the ratio of the speed of an object (such as an aircraft) to the speed of sound. If the Mach number is less than one, the flow is subsonic. If the Mach number is equal to one, the flow is transonic. I the Mach number is greater than one, the flow is supersonic. Write a function, with the following signature, that will compute and return the flow of the object function f- computeFlow (object_speed, sound_speed) Inputs object.speed: Speed of the object (km/s) sound_speed: Speed of sound (km/s) Output:f -1 if the flow is subsonic 0 if the flow is transonic 1 if the speed is supersonic 2-34 AM 5/09/2017 2 Type here to search