Euler’s equation for steady inviscid flow along a streamline — select the correct differential relation.

Difficulty: Easy

Correct Answer: dp/ρ + g * dz + v * dv = 0

Explanation:


Introduction / Context:
Euler’s equation is the inviscid (zero-viscosity) form of the momentum equation for fluid flow. When applied along a streamline under steady conditions for an incompressible fluid, it leads directly to the differential form that integrates to Bernoulli’s equation.


Given Data / Assumptions:

  • Steady flow, inviscid fluid, along a streamline.
  • Body force due to gravity acts in the −z direction (z positive upward).
  • Density ρ is constant (incompressible) for the differential form used here.


Concept / Approach:

Express the momentum balance per unit mass along a streamline. The pressure term appears as dp/ρ, elevation as g * dz, and the kinetic term as v * dv. The sum of these differential energy terms equals zero in the absence of losses or work input, yielding the familiar integrable form.


Step-by-Step Solution:

Write Euler (streamwise): dp/ρ + g * dz + v * dv = 0.Integrate to obtain Bernoulli: p/ρ + g * z + v²/2 = constant (per unit mass).Divide by g to write the head form if desired: p/(ρ g) + z + v²/(2 g) = constant.


Verification / Alternative check (if short method exists):

Dimensional analysis confirms dp/ρ has units of specific energy (m²/s²), same as g * dz and v * dv; options with ρ * dp or v² * dv are dimensionally inconsistent in this specific context.


Why Other Options Are Wrong:

(b) and (c) multiply the wrong terms by ρ; (d) uses v² * dv instead of v * dv; “none” is incorrect because (a) is the standard relation.


Common Pitfalls (misconceptions, mistakes):

Forgetting that the equation is per unit mass; confusing the integrated Bernoulli form with the differential Euler form.


Final Answer:

dp/ρ + g * dz + v * dv = 0

More Questions from Hydraulics

Discussion & Comments

No comments yet. Be the first to comment!
Join Discussion