-8D Static Free-stream pressure pressure Ps Stagnation pressure 4 to 8 holes +10% Static pressure Po Ps Stagnation pressure -10% 0° Differential 10° 20 Yaw angle 0 pressure transducer JO.Lg
-8D Static Free-stream pressure pressure Ps Stagnation pressure 4 to 8 holes +10% Static pressure Po Ps Stagnation pressure -10% 0° Differential 10° 20 Yaw angle 0 pressure transducer JO.Lg
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
Related questions
Question
When a pitot tube such as in Fig. is placed in a
supersonic flow, a normal shock will stand in front of
the probe. Suppose the probe reads p0 = 190 kPa and
p = 150 kPa. If the stagnation temperature is 400 K,
estimate the (supersonic) Mach number and velocity
upstream of the shock.
Transcribed Image Text:-8D
Static
Free-stream
pressure
pressure
Ps
Stagnation
pressure
4 to 8
holes
+10%
Static pressure
Po
Ps
Stagnation pressure
-10%
0°
Differential
10°
20
Yaw angle 0
pressure
transducer
JO.Lg
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