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7.10 A two-dimensional supersonic wing has the profile shown in Figure P7.10. At zero angle of attack, determine the drag force on the wing per unit length of span at Mach 2 and at Mach 4. Repeat for the lift force. Assume y = 1.4. M 1 = 0.2 m

7.10 A two-dimensional supersonic wing has the profile shown in Figure P7.10. At zero angle of attack, determine the drag force on the wing per unit length of span at Mach 2 and at Mach 4. Repeat for the lift force. Assume y = 1.4. M 1 = 0.2 m

Elements Of Electromagnetics
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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7.10 A two-dimensional supersonic wing has the profile shown in Figure P7.10. At zero angle of attack, determine the drag force on the wing per unit length of span at Mach 2 and at Mach 4. Repeat for the lift force. Assume y = 1.4. by installing sa teach COE) M 1 = 0.2 m L/2 1.2 m %3| L = 2.4 m
Transcribed Image Text:7.10 A two-dimensional supersonic wing has the profile shown in Figure P7.10. At zero angle of attack, determine the drag force on the wing per unit length of span at Mach 2 and at Mach 4. Repeat for the lift force. Assume y = 1.4. by installing sa teach COE) M 1 = 0.2 m L/2 1.2 m %3| L = 2.4 m
You have 2 shock waves and one expansion wave above the wing. What waves would you have to change or eliminate to increase the lift produced by this wing? How could you do this?
Transcribed Image Text:You have 2 shock waves and one expansion wave above the wing. What waves would you have to change or eliminate to increase the lift produced by this wing? How could you do this?
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