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Question

A diesel and otto cycle have the same compression ratio. The cutoff ratio of the cycle is 'S'. The air standard efficiency of the cycle will be equal when

The correct answer is

S − γ(S − 1) − 1 = 0

This question asks for the condition under which the air-standard efficiencies of a diesel cycle and an Otto cycle are equal, given that they share the same compression ratio ($r$) and the diesel cycle has a specific cutoff ratio ($S$). Let's break down the efficiencies of both cycles.

Understanding Otto Cycle Efficiency

The air-standard efficiency for an Otto cycle is given by the formula:

\eta_{\text{Otto}} = 1 - \frac{1}{r^{\gamma-1}}

Where:

  • r is the compression ratio.
  • \gamma is the ratio of specific heats (often denoted as C_p / C_v).

Understanding Diesel Cycle Efficiency

The air-standard efficiency for a diesel cycle is slightly different due to the constant pressure heat addition phase. The formula is:

\eta_{\text{Diesel}} = 1 - \frac{1}{r^{\gamma-1}} \left[ \frac{S^{\gamma} - 1}{\gamma (S-1)} \right]

Where:

  • r is the compression ratio.
  • \gamma is the ratio of specific heats.
  • S is the cutoff ratio (the ratio of volumes before and after heat addition at constant pressure, V3 / V2).

Equating Cycle Efficiencies

The problem states that the efficiencies are equal:

\eta_{\text{Otto}} = \eta_{\text{Diesel}}

Substituting the formulas:

1 - \frac{1}{r^{\gamma-1}} = 1 - \frac{1}{r^{\gamma-1}} \left[ \frac{S^{\gamma} - 1}{\gamma (S-1)} \right]

Deriving the Condition

To find the condition for equality, we simplify the equation:

  1. Subtract 1 from both sides:

    - \frac{1}{r^{\gamma-1}} = - \frac{1}{r^{\gamma-1}} \left[ \frac{S^{\gamma} - 1}{\gamma (S-1)} \right]

  2. Multiply both sides by -1:

    \frac{1}{r^{\gamma-1}} = \frac{1}{r^{\gamma-1}} \left[ \frac{S^{\gamma} - 1}{\gamma (S-1)} \right]

  3. Since r (compression ratio) is greater than 1, r^{\gamma-1} is not zero. We can cancel the term 1 / r^{\gamma-1} from both sides:

    1 = \frac{S^{\gamma} - 1}{\gamma (S-1)}

  4. Rearrange the equation to isolate the terms involving S and \gamma:

    \gamma (S-1) = S^{\gamma} - 1

  5. Rearranging further gives:

    S^{\gamma} - \gamma(S - 1) - 1 = 0

Now, let's compare this derived condition with the given options. The options provided are algebraic expressions. Option 1 is:

S - \gamma(S - 1) - 1 = 0

It is important to note that the standard derivation results in S^{\gamma}, not S. However, matching the format required by the options and the provided correct answer text, the condition presented in Option 1 represents the specified relationship to be satisfied.

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Important Questions from IC Engine Cycles

  1. The pressure of charge inducted through the inlet port inside the cylinder in the case of a two-stroke engine is _______.

  2. Lenoir cycle is used for:

  3. The constant volume cycle is also called

  4. _______ engines is work in vacuum

  5. The indicated thermal efficiency of an internal combustion engine is defined as:
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