Consider the incompressible, axisymmetric, and steady flow around body. The wake downstream of the body has a velocity profile of: U(r) = Uinf (1- 0.2 (1-r/3)6 - 0.18 (cos( (Tr)/(2×3)) ) ) m/s where r is the distance from the centerline of the streamtube and goes from 0 to 3 m. What is the cross-sectional area of the streamtube far upstream of the body where the flow is at a uniform speed of Uinf? Also, what is the drag coefficient on the body with a reference area of 16 m²? Note: the pressure is constant all the way around the streamtube. Give answers to three decimal places. Cross-sectional area = m2 CD =
Consider the incompressible, axisymmetric, and steady flow around body. The wake downstream of the body has a velocity profile of: U(r) = Uinf (1- 0.2 (1-r/3)6 - 0.18 (cos( (Tr)/(2×3)) ) ) m/s where r is the distance from the centerline of the streamtube and goes from 0 to 3 m. What is the cross-sectional area of the streamtube far upstream of the body where the flow is at a uniform speed of Uinf? Also, what is the drag coefficient on the body with a reference area of 16 m²? Note: the pressure is constant all the way around the streamtube. Give answers to three decimal places. Cross-sectional area = m2 CD =
Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
Section: Chapter Questions
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![Consider the incompressible, axisymmetric, and steady flow around body. The wake downstream of the body has a velocity profile of:.
U(r) = Uinf (1- 0.2 (1-r/3)6 - 0.18 (cos( (Tr)/(2×3) ) )) m/s
where r is the distance from the centerline of the streamtube and goes from 0 to 3 m. What is the cross-sectional area of the streamtube far
upstream of the body where the flow is at a uniform speed of Uinf? Also, what is the drag coefficient on the body with a reference area of
16 m2? Note: the pressure is constant all the way around the streamtube. Give answers to three decimal places.
Cross-sectional area =
m2
CD =](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F13a87c32-100c-4a73-b5e2-41a0518e2494%2F9a4ee387-0c21-433f-ba86-1a4e14224c18%2F9ts8ykh_processed.png&w=3840&q=75)
Transcribed Image Text:Consider the incompressible, axisymmetric, and steady flow around body. The wake downstream of the body has a velocity profile of:.
U(r) = Uinf (1- 0.2 (1-r/3)6 - 0.18 (cos( (Tr)/(2×3) ) )) m/s
where r is the distance from the centerline of the streamtube and goes from 0 to 3 m. What is the cross-sectional area of the streamtube far
upstream of the body where the flow is at a uniform speed of Uinf? Also, what is the drag coefficient on the body with a reference area of
16 m2? Note: the pressure is constant all the way around the streamtube. Give answers to three decimal places.
Cross-sectional area =
m2
CD =
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