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a jet aircraft flies at a speed of 550 mph at an altitude of 35,000 ft, where the temperature is minus 66°F and the specific heat ratio is k= 1.4 @ Determine the ratio of the speed of the aircraft. V, to that of the speed of sound, c, at the specified altitude. This ratio is called the mach number 1 Based on its Mach number, is the aircraft flying at subsonic or supersonic speed? C= √ k= heat ratio R= gas constant To absolute temperature KRT

a jet aircraft flies at a speed of 550 mph at an altitude of 35,000 ft, where the temperature is minus 66°F and the specific heat ratio is k= 1.4 @ Determine the ratio of the speed of the aircraft. V, to that of the speed of sound, c, at the specified altitude. This ratio is called the mach number 1 Based on its Mach number, is the aircraft flying at subsonic or supersonic speed? C= √ k= heat ratio R= gas constant To absolute temperature KRT

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
Problem 1.1MA
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(1) - (2) Open Gasoline Water 17 ft 3 ft
Transcribed Image Text:(1) - (2) Open Gasoline Water 17 ft 3 ft
utivn a jet aircraft flies at a speed of 550 mph at an altitude of 35,000 It, where the temperature is minus 66°F and the specific heat ratio is k= 1.4 @ Determine the ratio of the speed of the airchaft. V, to that of the speed of sound, c, at the specified altitude. This ratio is called the Mach number 1 Based on its Mach number, is the aircraft flying at subsonic or supersonic speed? C= k= heat ratio R= gas constant T = absolute temperature KRT
Transcribed Image Text:utivn a jet aircraft flies at a speed of 550 mph at an altitude of 35,000 It, where the temperature is minus 66°F and the specific heat ratio is k= 1.4 @ Determine the ratio of the speed of the airchaft. V, to that of the speed of sound, c, at the specified altitude. This ratio is called the Mach number 1 Based on its Mach number, is the aircraft flying at subsonic or supersonic speed? C= k= heat ratio R= gas constant T = absolute temperature KRT
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