Example 1 An airplane flies 800 km/hr. at an elevation of 10,000 m. in a standard atmosphere as shown in Figure. Determine the pressure at point (1) far ahead of the airplane, the pressure at the stagnation point on the nose of the airplane, point (2), and the pressure difference indicated by a Pitot static probe attached to the fuselage. Aecle
Example 1 An airplane flies 800 km/hr. at an elevation of 10,000 m. in a standard atmosphere as shown in Figure. Determine the pressure at point (1) far ahead of the airplane, the pressure at the stagnation point on the nose of the airplane, point (2), and the pressure difference indicated by a Pitot static probe attached to the fuselage. Aecle
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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
Transcribed Image Text:Example 1
An airplane flies 800 km/hr. at an elevation of 10,000 m. in a standard
atmosphere as shown in Figure. Determine the pressure at point (1) far
ahead of the airplane, the pressure at the stagnation point on the nose of the
airplane, point (2), and the pressure difference indicated by a Pitot static
probe attached to the fuselage.
Acceleatin
Gra
P
Desin.
Aiude Temp
-1.000
1 ES 13e E.
2150
00
30
200
12 E-S
1013 ES 1 225E 17 E-5
175 E-S
17 E-S
L00
2000
3.000
9 E4 112 E.
19 E
1012 E4 9) E-I 1 E -S
61 E4 IN E-I 161E-S
14 E-I 1 E-S
1.595 E-S
I E4 S00 E-I 11 E-S
15 E4 S.25E-I 1527E-S
140 E-S
4135 E-1 14s E-S
194 E-1 1422 E-5
10
174
4.000
1000
140 E4
4722 4
6.000
-23
(2)
1.000
.000
10.000
979
9776
4671 E-I
10 E4
260 E4
(1)
V =800km/h
15.000
20.000
25.000
J0.000
-5630
560
-510
464
-220
-250
1211 E4
59 E SI E- 142 E-S
400 E-2
134E-2
14 E-S
1475 E-5
1001 E-S
25 E
Pitot-static tube
9715
2871 E+2
40.000
S0.000
60.000
70.000
3996 E-)
797 E1 1027 E- 104 E-S
3.007 E-4
654
4
154 E-S
5221 E.
1052 E.
-5357
2 E-5
136 E-S
14 E-5
B0.000
9.504
1321 E-5
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