Q2/ Answer the following: 1) Separation in flow past a solid object is caused by (a) a favourable (negative ) pressure gradient (b) an adverse ( positive ) pressure gradient (c) the boundary layer thickness reducing to zero 2) In the design, we have to delay the separation point in order to reduce wake size (T/F) 3) Define Mach number, boundary layer and shock wave. 4) when --- , the flow is accelerates if the cross sectional area is increases (а) М<1 (b) М> 1 (c) M =1
Q2/ Answer the following: 1) Separation in flow past a solid object is caused by (a) a favourable (negative ) pressure gradient (b) an adverse ( positive ) pressure gradient (c) the boundary layer thickness reducing to zero 2) In the design, we have to delay the separation point in order to reduce wake size (T/F) 3) Define Mach number, boundary layer and shock wave. 4) when --- , the flow is accelerates if the cross sectional area is increases (а) М<1 (b) М> 1 (c) M =1
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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![Q2/ Answer the following:
1) Separation in flow past a solid object is caused by
(a) a favourable (negative ) pressure gradient
(b) an adverse ( positive ) pressure gradient
(c) the boundary layer thickness reducing to zero
2) In the design, we have to delay the separation point in order to reduce wake size (T/F)
3) Define Mach number, boundary layer and shock wave.
4) when
the flow is accelerates if the cross sectional area is increases
(a) M<1
(b) M > 1
(c) M =1](/v2/_next/image?url=https%3A%2F%2Fcontent.bartleby.com%2Fqna-images%2Fquestion%2F86cd17be-79cd-447c-b847-4cef9b7c15c4%2F29f2f826-ca6f-41e4-bcb5-fcf5fb3fb8d2%2Fyw74u3j_processed.jpeg&w=3840&q=75)
Transcribed Image Text:Q2/ Answer the following:
1) Separation in flow past a solid object is caused by
(a) a favourable (negative ) pressure gradient
(b) an adverse ( positive ) pressure gradient
(c) the boundary layer thickness reducing to zero
2) In the design, we have to delay the separation point in order to reduce wake size (T/F)
3) Define Mach number, boundary layer and shock wave.
4) when
the flow is accelerates if the cross sectional area is increases
(a) M<1
(b) M > 1
(c) M =1
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