Initially contains Air: P1 = 30 lbf/in^2 T1 = 540 °F V1 = 4 ft^3 Second phase of process involving Air to a final state: P2 = 20 lbf/in^2 V2 = 4.5 ft^3 Wheel transfers energy TO the air by WORK at 1 Btu. Energy transfers TO the air by HEAT at 12 Btu. Ideal Gas Behavior. Wow=-1 Btu Vpw Q = -12 Btu Determine whether the propeller's work is done BY the system or On the system. Air Wpist = ? Initially, p₁ = 30 lbf/in.2, T₁ = 540°F, V₁ = 4 ft³. Finally, p2 = 20 lbf/in.², V₂ = 4.5 ft³.

Elements Of Electromagnetics
7th Edition
ISBN:9780190698614
Author:Sadiku, Matthew N. O.
Publisher:Sadiku, Matthew N. O.
ChapterMA: Math Assessment
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**Initial Conditions:**

- Pressure (P1): 30 lbf/in²
- Temperature (T1): 540 °F
- Volume (V1): 4 ft³

**Final Conditions:**

- Pressure (P2): 20 lbf/in²
- Volume (V2): 4.5 ft³

**Energy Transfer Details:**

- Work done by the wheel on the air: 1 Btu (transfers energy TO the air)
- Heat added to the air: 12 Btu

**Process Assumptions:**

- The behavior of the air follows ideal gas laws.

**Diagram Explanation:**

The diagram illustrates a system with air confined in a cylinder, equipped with a piston and a propeller. The propeller does work on the system (-1 Btu), while heat energy of -12 Btu is transferred out of the system (Q).

**Objective:**

- **Determine whether the propeller's work is done BY the system or ON the system.**

In the context of this thermodynamic problem, analyze the work interactions to derive the correct direction of energy transfer concerning the air system.
Transcribed Image Text:**Initial Conditions:** - Pressure (P1): 30 lbf/in² - Temperature (T1): 540 °F - Volume (V1): 4 ft³ **Final Conditions:** - Pressure (P2): 20 lbf/in² - Volume (V2): 4.5 ft³ **Energy Transfer Details:** - Work done by the wheel on the air: 1 Btu (transfers energy TO the air) - Heat added to the air: 12 Btu **Process Assumptions:** - The behavior of the air follows ideal gas laws. **Diagram Explanation:** The diagram illustrates a system with air confined in a cylinder, equipped with a piston and a propeller. The propeller does work on the system (-1 Btu), while heat energy of -12 Btu is transferred out of the system (Q). **Objective:** - **Determine whether the propeller's work is done BY the system or ON the system.** In the context of this thermodynamic problem, analyze the work interactions to derive the correct direction of energy transfer concerning the air system.
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