By using normal shock tables 67 Shock Wave in a Converging-Diverging NozzleIf the air flowing through the converging-diverging nozzle of Example 17-7 experiences a normal shock wave at the nozzle exit plane (Fig. 17-36), determinethe following after the shock: (a) the stagnation pressure, static pressure, statictemperature, and static density; (b) the exit velocity; and Approximate the flow assteady, one-dimensional, and isentropic with k = 1.4 from the nozzle. inlet to theshock location..m=286kg/sShock wave2Ma₁ = 2Po1.0 MPaP₁ = 0.1278 MPaT₁ = 444.5 KPi= 1.002 kg/m³FIGURE 17-36Schematic for Example 17-9.

Ma1 = 2 P01 = 1.0 MPa m2 = 86 kg/s P1 = 0.1278 MPa T₁ = 444.5 K ρ1 = 1.002 kg/m

Shock Wave in a Converging-Diverging Nozzle the air flowing through the converging-diverging nozzle of Example 17- experiences a normal shock wave at the nozzle exit plane (Fig. 17-36), determine The following after the shock: (a) the stagnation pressure, static pressure, static emperature, and static density; (b) the exit velocity; and Approximate the flow as steady, one-dimensional, and isentropic with k = 1.4 from the nozzle inlet to the shock location. = 2,86 kg/s Shock wave 2 Ma₁ = 2 Pol=1.0 MPa P₁ = 0.1278 MPa T₁ = 444.5 K Pi= 1.002 kg/m³ FIGURE 17-36 Schematic for Example 17-9.

Shock Wave in a Converging-Diverging Nozzle the air flowing through the converging-diverging nozzle of Example 17- experiences a normal shock wave at the nozzle exit plane (Fig. 17-36), determine The following after the shock: (a) the stagnation pressure, static pressure, static emperature, and static density; (b) the exit velocity; and Approximate the flow as steady, one-dimensional, and isentropic with k = 1.4 from the nozzle inlet to the shock location. = 2,86 kg/s Shock wave 2 Ma₁ = 2 Pol=1.0 MPa P₁ = 0.1278 MPa T₁ = 444.5 K Pi= 1.002 kg/m³ FIGURE 17-36 Schematic for Example 17-9.

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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