abcdefghjklmnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnop xyz A converging nozzle has a throat area of 8.5 x10 m². Given that the stagnation air pressure and abcdefgh abcdefgh abcdefgh xyz temperature are 185 kPa and 450 K, respectively, and k is 1.4. abcdefghijklmnopqrstuvwxyz abcdefghij mnopqrstuvwxyz abcdefgh abcdefgh yz (a) Determine the critical throat pressure. abcdefghijklmnopqrstuvwxyz abcdefgh abcdefgh abcdefgh abcdefgh abcdefgh abcdefghijklmnopqrstu abcdefghijklmnopqrstuvw abcdefghijklmno Imnopqrstuvwxyz abcdefghijklmnopqrstuv nopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqrstuve yz (b) Determine the exit Mach number, exit pressure and mass flow if the back pressure is 115 abcdefgh abcdefgh abcdefgh vwxyzkPa. State whether the flow is choked or not, abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrst abcdefghijklmnopqrst mnopqrstuvwxyz abcdefgh abcdefgh mnopqrstuvwxyz abcdefgh abcdefgh abcdefghijkimnopqrstuvwxyz abeciefghikimnopqrstuvwxyz abcdefgh klmnopqrstuvwxyz xyz (c) Determine the exit pressure if the back pressure is 80 kPa. State whether the flow is choked abcdefgh vwxyz or not. abcdefghijklmnopqrstuvwxyz mnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvw abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqr klmnopqrstuvwxyz pqrstuv abcdefghijklmnopqrstuvy

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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Fluid dynamics-COMPRESSIBLE FLOW.
Ignore that abcd
stuvwxyz
abcdeighijkimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqrs
abcdefghijklmnopqrstuvw
abcdefghijklmnopqrstuv
abcdefghijklmnopqrstuvwxyz
abcdefghijkimnopqrstuvwxyz
nnopqrstuvwxyz A converging nozzle has a throat area of 8.5 x 104 m². Given that the stagnation air pressure and abcdefghijklmn
inopqrstuvwxyz temperature are 185 kPa and 450 K, respectively, and k is 1.4. abcdefghijklmnopqrstuvwxyz abcdefghijklmno
abcdefgh
abcdefgh
abcdefgh
abcdefgh
abcdefghijkimnopqrstuvwxyz
inopqrstuvwxyz (a) Determine the critical throat pressure. abcdefghijklmnopqrstuvwxyz
abcdefghijkimnopqrstuvwxyz
bcdefghijklmnopqrstuvwxyz
abcdefgh
abcdefgh
abcdefgh
abcdefgh
abcdefgh
abcdefghijklmnopqrstu
abcdefghijkimnopqrstuvwxyz
abcdefghijkimnopqrstuvwxyz
abcdefghijklmnopqrstuvwxyz
nnopqrstuvwxyz (b) Determine the exit Mach number, exit pressure and mass flow if the back pressure is 115 abcdefghijklmn
abcdefgh
abcdefgh
ijklmnopqrstuvwxyzkPa. State whether the flow is choked or not. abcdefghijklmnopqrstuvwxyz
abcdefghijklmnopqrstuvwxy
abcdefgh
abcdefghijklmnopqrst
abcdefgh
abcdefgh
abcdefgh
abcdefghikimnopqrstuvwxyz.
abcdefghijklmnopqrstuvwxyz
abcdefghijklmnopqrstuvwxyz abcdefghi|kimnopqrstuvwxyz
abcdefghijkimnopqrstuvwxyz
abcdefghijklmnouvwxy
abcdefghi kimnopqrstuvwxyz
abcdefghijklmnopqrstuvwxyz
abcdefghjklmnopqrstuvwxyz abcdefghi kimnopqrstuvwxyz
abcdefgh
abcdefghijklmnopqrstuvwxyz
proporstuvwxyz (c) Determine the exit pressure if the back pressure is 80 kPa. State whether the flow is choked abcdefghijklmn
fghijklmnopqrstuvwxyz abcdefgh
jklmnopqrstuvwxyz or not. abcdefghijklmnopqrstuvwxyz
abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz
hijklm
abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqr
nopqrstuvwxyz
abcdefghijkimnopqrstuvwxyz
ijklmi
aucdefghijklmnopqrstuvwxyz
abcdefchikimnoparstuvwxyz
Transcribed Image Text:Fluid dynamics-COMPRESSIBLE FLOW. Ignore that abcd stuvwxyz abcdeighijkimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqrs abcdefghijklmnopqrstuvw abcdefghijklmnopqrstuv abcdefghijklmnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz nnopqrstuvwxyz A converging nozzle has a throat area of 8.5 x 104 m². Given that the stagnation air pressure and abcdefghijklmn inopqrstuvwxyz temperature are 185 kPa and 450 K, respectively, and k is 1.4. abcdefghijklmnopqrstuvwxyz abcdefghijklmno abcdefgh abcdefgh abcdefgh abcdefgh abcdefghijkimnopqrstuvwxyz inopqrstuvwxyz (a) Determine the critical throat pressure. abcdefghijklmnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz bcdefghijklmnopqrstuvwxyz abcdefgh abcdefgh abcdefgh abcdefgh abcdefgh abcdefghijklmnopqrstu abcdefghijkimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz nnopqrstuvwxyz (b) Determine the exit Mach number, exit pressure and mass flow if the back pressure is 115 abcdefghijklmn abcdefgh abcdefgh ijklmnopqrstuvwxyzkPa. State whether the flow is choked or not. abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvwxy abcdefgh abcdefghijklmnopqrst abcdefgh abcdefgh abcdefgh abcdefghikimnopqrstuvwxyz. abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz abcdefghi|kimnopqrstuvwxyz abcdefghijkimnopqrstuvwxyz abcdefghijklmnouvwxy abcdefghi kimnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz abcdefghjklmnopqrstuvwxyz abcdefghi kimnopqrstuvwxyz abcdefgh abcdefghijklmnopqrstuvwxyz proporstuvwxyz (c) Determine the exit pressure if the back pressure is 80 kPa. State whether the flow is choked abcdefghijklmn fghijklmnopqrstuvwxyz abcdefgh jklmnopqrstuvwxyz or not. abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz abcdefghijklmnopqrstuvwxyz hijklm abcdefghijkimnopqrstuvwxyz abcdefghijklmnopqr nopqrstuvwxyz abcdefghijkimnopqrstuvwxyz ijklmi aucdefghijklmnopqrstuvwxyz abcdefchikimnoparstuvwxyz
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