Blasius limit
At \(M_e \to 0\), adiabatic wall, \(\beta = 0\) (flat plate), the compressible Falkner-Skan system reduces to the classical incompressible Blasius equation:
The expected wall shear in the Levy-Lees non-dimensionalization is \(f''(0) = 0.4696\).
Why is the Levy-Lees value 0.4696, not the Blasius value 0.3321?
The Levy-Lees similarity coordinates are defined as:
For a flat plate with uniform edge conditions \(\xi = \rho_e \mu_e u_e x\), so \(\sqrt{2\xi} = \sqrt{2\rho_e \mu_e u_e x}\) and the wall-normal coordinate becomes:
At \(M_e \to 0\), \(\rho \to \rho_e\), so the integral reduces to \(\rho_e y\):
where \(\nu = \mu_e/\rho_e\). So:
Both systems describe the same physical velocity ratio \(u/u_e = f'\), so the two stream functions are related by:
Differentiating both sides with respect to \(\eta_{LL}\) via the chain rule:
Evaluating at the wall (\(\eta_{LL} = 0\)):
At \(M_e \to 0\), adiabatic wall, \(\tau = T/T_e \approx 1\) everywhere.
Results
Profiles of \(f'(\eta)\), \(f''(\eta)\), and \((\tau - 1) \times 10^n\) (scaled so the deviation is \(O(1)\)). Dashed lines mark \(f''(0)_\text{ref} = 0.4696\) and \(\tau - 1 = 0\).




Both \(|f''(0) - f''(0)_\text{ref}|\) and \(\max|\tau - 1|\) converge to zero as \(M_e \to 0\):

Both errors converge monotonically to zero as \(M_e \to 0\), confirming that the solver correctly recovers the Blasius solution in the incompressible limit.
Run
The verification script is
vnv/verification/falkner_skan/blasius/verification_blasius.py.