8. Air is flowing through a wide channel at a Mach number of 2 at a pressure of 140 kPa. The upper wall of the channel turns through an angle of 8° "away" from the flow leading to the generation of an expansion wave, while the lower wall of the channel turns through an angle of 6° "away" from the flow also leading to the generation of an expansion wave. The two expansion waves interact and "pass through" each other. Find the Mach number, flow direction, and pressure just downstream of this interaction.

Elements Of Electromagnetics
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Author:Sadiku, Matthew N. O.
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expansión Wave.
7.8. Air is flowing through a wide channel at a Mach number of 2 at a pressure of
140 kPa. The upper wall of the channel turns through an angle of 8° "away"
from the flow leading to the generation of an expansion wave, while the lower
wall of the channel turns through an angle of 6° "away" from the flow also
leading to the generation of an expansion wave. The two expansion waves
interact and "pass through" each other. Find the Mach number, flow direction,
and pressure just downstream of this interaction.
7.9. A symmetrical double-wedge shaped body with an included angle of 15° is
aligned with an air flow in which the Mach number is 3 and the pressure is
20 kPa. The flow situation is, therefore, as shown in Fig. P7.9. Find the pres-
sures acting on the surfaces of the body.
M = 3
FIGURE P7.9
15°
15°
p= 20 kPa
7.10. A simple wing may be modeled as a 0.3 m wide flat plate set at an angle of 3 to
an airflow at a Mach number of 3, the pressure in this flow being 40 kPa.
Assuming
Transcribed Image Text:expansión Wave. 7.8. Air is flowing through a wide channel at a Mach number of 2 at a pressure of 140 kPa. The upper wall of the channel turns through an angle of 8° "away" from the flow leading to the generation of an expansion wave, while the lower wall of the channel turns through an angle of 6° "away" from the flow also leading to the generation of an expansion wave. The two expansion waves interact and "pass through" each other. Find the Mach number, flow direction, and pressure just downstream of this interaction. 7.9. A symmetrical double-wedge shaped body with an included angle of 15° is aligned with an air flow in which the Mach number is 3 and the pressure is 20 kPa. The flow situation is, therefore, as shown in Fig. P7.9. Find the pres- sures acting on the surfaces of the body. M = 3 FIGURE P7.9 15° 15° p= 20 kPa 7.10. A simple wing may be modeled as a 0.3 m wide flat plate set at an angle of 3 to an airflow at a Mach number of 3, the pressure in this flow being 40 kPa. Assuming
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