solve the following required A)The exhaust area in m^2 ?B)The exhaust gas density in kg/m^3 ? A static thrust stand as sketched in the figure shown is used for testing a jet engine. The following conditions are known for a typical test: the fuel enters at a flow rate of5 kg/s with approximate zero velocity. Intake air velocity is 215 m/s and exhaust gas velocity is 500 m/s; intake cross-sectional area is 1.2 m^2; intake static gaugepressure -30 kPa; intake air density is 0.9 kg/m^3 and exhaust static temperature 800 K; exhaust static pressure 0 kPa. If the atmospheric pressure is 100 kPa, theconstant for air and gas is R= 287 J/(kg. K). The exhaust area in m^2 is:Control volumeFuel inletSelect one:Patra. 1.07P2U2P1O b. 1.09c. 1.04Section (2)Section (1) A static thrust stand as sketched in the figure shown is used for testing a jet engine. The following conditions are known for a typical test: the fuel enters at a flow rate of5 kg/s with approximate zero velocity. Intake air velocity is 215 m/s and exhaust gas velocity is 500 m/s; intake cross-sectional area is 1.2 m^2; intake static gaugepressure -30 kPa; intake air density is 0.9 kg/m^3 and exhaust static temperature 800 K; exhaust static pressure 0 kPa. If the atmospheric pressure is 100 kPa, theconstant for air and gas is R= 287 J/(kg. K). The exhaust gas density in kg/m^3 is:Control volumeFuel inletSelect one:Patma. 0.44P2U2P1O b. 0.84O c. 1.00Section (2)Section (1)

A) option a is correct exhaust area is 1.07 m² B) option a is correct exhaust density is 0.44 kg/ m3…

A static thrust stand as sketched in the figure shown is used for testing a jet engine. The following conditions are known for a typical test: the fuel enters at a flow rate of 5 kg/s with approximate zero velocity. Intake air velocity is 215 m/s and exhaust gas velocity is 500 m/s; intake cross-sectional area is 1.2 m^2; intake static gauge pressure -30 kPa; intake air density is 0.9 kg/m^3 and exhaust static temperature 800 K; exhaust static pressure 0 kPa. If the atmospheric pressure is 100 kPa, the constant for air and gas is R= 287 /(kg. K). The exhaust area in m^2 is: Control volume Fuel inlet Select one: Patr a. 1.07 P1 b. 1.09 O c. 1.04 Section (2) Section (1)

A static thrust stand as sketched in the figure shown is used for testing a jet engine. The following conditions are known for a typical test: the fuel enters at a flow rate of 5 kg/s with approximate zero velocity. Intake air velocity is 215 m/s and exhaust gas velocity is 500 m/s; intake cross-sectional area is 1.2 m^2; intake static gauge pressure -30 kPa; intake air density is 0.9 kg/m^3 and exhaust static temperature 800 K; exhaust static pressure 0 kPa. If the atmospheric pressure is 100 kPa, the constant for air and gas is R= 287 /(kg. K). The exhaust area in m^2 is: Control volume Fuel inlet Select one: Patr a. 1.07 P1 b. 1.09 O c. 1.04 Section (2) Section (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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