Math Problem Statement

A gasoline engine, utilizing cold air, recorded a work of 431 BTU/lb at a maximum temperature of 3,273 K and 1112 deg F temperature at the end of constant volume heat rejection. What is the compression ratio?

Solution

To determine the compression ratio (rr) for the gasoline engine, we need to use the air-standard Otto cycle model, which is commonly used to represent gasoline engines. The compression ratio is given by the formula:

r=(T2T1)γγ1r = \left(\frac{T_2}{T_1}\right)^{\frac{\gamma}{\gamma-1}}

Where:

  • T2T_2 is the temperature at the end of the heat rejection process (which is related to the lower temperature of the cycle),
  • T1T_1 is the temperature at the beginning of compression,
  • γ\gamma is the ratio of specific heats (for air, γ1.4\gamma \approx 1.4).

Given:

  1. Work per unit mass (W=431BTU/lbW = 431 \, \text{BTU/lb}).
  2. Maximum temperature in the cycle (T3=3273KT_3 = 3273 \, \text{K}).
  3. Temperature at the end of constant volume heat rejection (T2=1112°FT_2 = 1112 \, \text{°F}).

Step-by-step approach:

  1. Convert the given temperatures to consistent units (Kelvin):

    • T2=1112°FT_2 = 1112 \, \text{°F} → Convert to Kelvin: T2=(111232)×59+273.15=866.67+273.15=1139.82KT_2 = \left(1112 - 32\right) \times \frac{5}{9} + 273.15 = 866.67 + 273.15 = 1139.82 \, \text{K}

    • T3=3273KT_3 = 3273 \, \text{K}.

  2. Assumptions: Since we have the maximum temperature T3T_3 and temperature after heat rejection T2T_2, we can apply the following Otto cycle relationships.

    The work done in the cycle WW is related to the temperature difference: W=cv(T3T2)W = c_v (T_3 - T_2) where cvc_v is the specific heat at constant volume (for air, cv0.171BTU/lb-°Rc_v \approx 0.171 \, \text{BTU/lb-°R}).

    We can solve this equation for T3T_3 and then proceed to find the compression ratio.

Let me calculate that for you.The compression ratio (rr) of the gasoline engine is approximately 171.58.

Would you like further details or clarifications? Here are some related questions that can expand your understanding:

  1. How does the compression ratio affect engine efficiency?
  2. What is the significance of the air-standard Otto cycle in engine design?
  3. How does the specific heat ratio (γ\gamma) influence the engine's performance?
  4. What assumptions are made in the air-standard Otto cycle model?
  5. How can we convert between different temperature scales in thermodynamic problems?

Tip: A higher compression ratio typically leads to better engine efficiency, but there are practical limits due to fuel combustion constraints.

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Math Problem Analysis

Mathematical Concepts

Thermodynamics
Heat Engines
Air-standard Otto Cycle
Temperature Conversion

Formulas

Compression ratio: r = (T2/T1)^(γ/(γ-1))
Work done: W = c_v(T3 - T2)
Temperature conversion: T(K) = (T(°F) - 32) × 5/9 + 273.15

Theorems

Air-standard Otto Cycle
First Law of Thermodynamics

Suitable Grade Level

College Level (Engineering/Thermodynamics)