Example 1An airplane flies 800 km/hr. at an elevation of 10,000 m. in a standardatmosphere as shown in Figure. Determine the pressure at point (1) farahead of the airplane, the pressure at the stagnation point on the nose of theairplane, point (2), and the pressure difference indicated by a Pitot staticprobe attached to the fuselage.AcceleatinGraPDesin.Aiude Temp-1.0001 ES 13e E.2150003020012 E-S1013 ES 1 225E 17 E-5175 E-S17 E-SL0020003.0009 E4 112 E.19 E1012 E4 9) E-I 1 E -S61 E4 IN E-I 161E-S14 E-I 1 E-S1.595 E-SI E4 S00 E-I 11 E-S15 E4 S.25E-I 1527E-S140 E-S4135 E-1 14s E-S194 E-1 1422 E-5101744.0001000140 E44722 46.000-23(2)1.000.00010.00097997764671 E-I10 E4260 E4(1)V =800km/h15.00020.00025.000J0.000-5630560-510464-220-2501211 E459 E SI E- 142 E-S400 E-2134E-214 E-S1475 E-51001 E-S25 EPitot-static tube97152871 E+240.000S0.00060.00070.0003996 E-)797 E1 1027 E- 104 E-S3.007 E-46544154 E-S5221 E.1052 E.-53572 E-5136 E-S14 E-5B0.0009.5041321 E-5

Given Data Velocity of plane is: v=800 km/h=222.22 m/s Height of the plane is: h=10000 m Density…

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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