Quiz 4.docx - Cours 202040 Fall 2020 AVIA 305-D01 e LUO...

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Cours e 202040 Fall 2020 AVIA 305-D01 LUO Test Test 4 Starte d Question 1 2.5 out of 2.5 points In Subsonic flight the air is considered to be Question 2 2.5 out of 2.5 points A Normal shock wave will have what effect on velocity and Mach number? Question 32.5 out of 2.5 pointsAircraft speeds where the airflow around the aircraft ranges between Mach 0.7 and Mach 1.3 is Question 4 2.5 out of 2.5 points A "stable" aircraft wing design is one where the Question 52.5 out of 2.5 pointsNormally, the ailerons are used to produce rolling moments, however, the __________ can also produce rolling moments Question 6 0 out of 2.5 points
Weight and balance of airplanes is important because Question 7 0 out of 2.5 points A “neutral” aircraft wing design is one where the

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