Knowledge card
Skin Friction Coefficient Cf
Mathematical Modelling — Fluid Dynamics & Heat TransferContinuum mechanics; boundary-layer similarity theory
Symbol
CfThe wall shear stress, proportional to f″(0) — the drag the plate exerts on the flow.
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In words:equalsminus.
Open full derivation chain: 3 stepsDerivation
- 1
Open Step 1: Given / definition · Use the standard local skin-friction coefficient C_f = τ_w/(½ρ_fU_w²), with the complete trunca…
Use the standard local skin-friction coefficient C_f = τ_w/(½ρ_fU_w²), with the complete truncated Powell–Eyring wall stress. The factor ½ is therefore retained on the scaled left-hand side.Given / definition Defining ruleThe starting relation of a derivation — the definition or established equation every later step transforms; it justifies no change itself.Level 0 · more availableBrief — named quantitiesAbout levels
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To go deeper still, open any quantity in the reading as its own concept card — it carries its own derivation and its own depth ladder.
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- 2
Open Step 2: Similarity transformation · Substitute the wall shear-rate map ∂u/∂y(0) = U_w√(c/(ν_f(1−γt)))f″(0) into both wall-stress pa…
Substitute the wall shear-rate map ∂u/∂y(0) = U_w√(c/(ν_f(1−γt)))f″(0) into both wall-stress parts: the dimensional wall shear rate becomes the dimensionless wall shear f″(0), the coefficients carried.Similarity transformation Defining ruleu(x, y, t) = U(x, t)·F(η), η = y/δ(x, t)A change of variables that collapses several independent variables into one similarity coordinate, reducing a PDE to an ODE; each substituted term splits into a dimensional scale times a dimensionless group.Substitution · ∂u/∂y=U_w√(c/(ν_f(1−γt)))f″ Operand nodeShear-rate MapOne wall-normal derivative of the velocity map: each ∂/∂y contributes one similarity length factor.Substitution: The operand (a map or model) replaces the source directly.Open term-change ledger: 2 records
Open record 1: (μ+1/(βς))∂u/∂y(0) → (μ+1/(βς))f″(0)
Consumes:L0Produces:L0The wall shear-rate map ∂u/∂y(0) = U_w√(c/(ν_f(1−γt)))f″(0) turns the linear wall stress into the effective linear viscosity times the dimensionless wall shear f″(0).(μ+1/(βς))f″(0)Resulting expressionMapped Linear Wall ShearThe linear wall stress after substituting the wall shear-rate map — the effective linear viscosity times the dimensionless wall shear f″(0), before the coefficient is named.Open record 2: (1/(6βς³))(∂u/∂y(0))³ → (1/(6βς³))f″(0)³
Consumes:L0Produces:L0The same map (cubed) turns the cubic wall stress into the cubic coefficient times f″(0)³.(1/(6βς³))f″(0)³Resulting expressionMapped Cubic Wall ShearThe cubic wall stress after substituting the wall shear-rate map — the cubic coefficient times f″(0)³, before it is named εδ/3.Level 0 · more availableBrief — named quantitiesAbout levels
Why the levels load one at a time
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- ★
Open Step 3: Parameter definition · Form ½Re_x^½C_f and identify the coefficients: the linear coefficient becomes φ_μ+ε and the cub…
Form ½Re_x^½C_f and identify the coefficients: the linear coefficient becomes φ_μ+ε and the cubic coefficient becomes εδ/3. Equivalently, Re_x^½C_f is twice the right-hand side.Parameter definition Defining ruleΠ ≔ (grouped physical quantities)Naming a recurring group of quantities as a single parameter (A ≔ γ/c, M ≔ σB₀²/(ρc), …), replacing the group by its name.Open term-change ledger: 2 records
Open record 1: (μ+1/(βς))f″(0) → (φ_μ+ε)f″(0)
Consumes:L0Produces:L0The effective linear viscosity (μ + 1/(βς)), scaled, is DEFINED as the viscous–elastic numerator φ_μ + ε (ε the first Powell–Eyring parameter), giving (φ_μ + ε)f″(0).(φ_μ+ε)f″(0)Resulting expressionLinear Wall-shear TermThe Newtonian-plus-linear-Powell–Eyring part of the wall shear — the viscous–elastic numerator times the wall shear f″(0).Open record 2: (1/(6βς³))f″(0)³ → (εδ/3)f″(0)³
Consumes:L0Produces:L0The cubic coefficient (1/(6βς³)), scaled, is DEFINED as εδ/3 through the Powell–Eyring parameters ε and δ, giving the shear-thinning correction (εδ/3)f″(0)³.(εδ/3)f″(0)³Resulting expressionNonlinear Wall-shear CorrectionThe shear-thinning correction to the wall stress — the nonlinear coefficient times the cubed wall shear.Level 0 · more availableBrief — named quantitiesAbout levels
Why the levels load one at a time
Only level 0 travels with this article. The complete expansion is several megabytes, so deeper levels are fetched one at a time when you ask for them — and how deep it goes is not known until you get there.
To go deeper still, open any quantity in the reading as its own concept card — it carries its own derivation and its own depth ladder.
How many levels remain is not yet known — the depth is discovered one level at a time.
Numerical solution · Skin Friction Coefficient Cf
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Equation workspace
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Domain Analysis
Unit status, dimensional trails, per-step checks, and custom unit expressions.
Domain Analysis
Unit status, dimensional trails, per-step checks, and custom unit expressions.
Step-by-step unit check (3 steps)
Step 1 given
Expand checked this step.Step 2 similarity_transform
Expand checked this step.Step 3 parameter_definition
Expand checked this step.
Try your own — the unit calculator
Ever wondered whether a formula “adds up”? This tool answers one plain question: do the units match? Pick a couple of quantities (distance, time, a speed…), join them with ×, ÷, +, or =, and press Run. It works out the resulting unit — for example distance ÷ time gives a speed, LT⁻¹ (metres per second) — and flags anything that can’t be right, like adding a length to a time.
Reads as: Cf
“Cf” is analysed by expanding its full defining equation (its children and their relations), not as a bare symbol. Use Check this concept’s units above for the same result.
Mathematical Analysis
Object type, lawful operations, conditions, comparisons, and derivation-step checks.
Mathematical Analysis
Object type, lawful operations, conditions, comparisons, and derivation-step checks.
Check one step at a time (3 steps)
Step 1 — given
Step 2 — similarity transform
Step 3 — parameter definition
Also known as:Cf
Essence
S1The wall stress after substitution: (μ + 1/(βς))f″(0) − (1/(6βς³))f″(0)³, before the parameters are named.
- S1.1essence(μ+1/(βς))f″(0) reduced by (1/(6βς³))f″(0)³.
- S1.2essence½Re_x^½C_f set equal to ((μ+1/(βς))f″(0) − (1/(6βς³))f″(0)³).
Dimension I
Definition
What it is — and what it is not
- What it is
- S2The dimensionless wall shear (drag).
- S3The standard scaled group is ½Re_x^½C_f, derived from τ_w = (μ_hnf+1/(βς))u_y − u_y³/(6βς³) at y=0.
- S3.1essence(μ+1/(βς))∂u/∂y(0) reduced by (1/(6βς³))(∂u/∂y(0))³.
- S3.2essence½Re_x^½C_f set equal to ((μ+1/(βς))∂u/∂y(0) − (1/(6βς³))(∂u/∂y(0))³).
- Wisdoms
- S4The standard result: ½Re_x^½C_f = (φ_μ+ε)f″(0) − (εδ/3)f″(0)³.
- S4.1essence(φ_μ+ε)f″(0) reduced by (εδ/3)f″(0)³.
- S4.2essence½Re_x^½C_f set equal to ((φ_μ+ε)f″(0) − (εδ/3)f″(0)³).
- S4The standard result: ½Re_x^½C_f = (φ_μ+ε)f″(0) − (εδ/3)f″(0)³.
- Attributes
- S5It is proportional to f″(0) from the momentum solution.
- Common misconceptions
- S6Writing Re_x^½C_f=(1+ε)f″(0)−… both drops the hybrid viscosity ratio and hides the coefficient convention. For C_f=τ_w/(½ρ_fU_w²), the correct group is ½Re_x^½C_f=(φ_μ+ε)f″(0)−(εδ/3)f″(0)³. [1.1]
Dimension II
In practice
How to deal with it
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