1. SmithA. M. O. “Transition, Pressure Gradient and Stability Theory,” Douglas Aircraft Co. Rept. ES 26388, Santa Monica, CA, 1956.
2. van IngenJ. “A Suggested Semi-Empirical Method for the Calculation of the Boundary Layer Transition Region,” Technische Hogeschool Delft, Rapport VTH-74, Vliegtuigbouwkunde, Delft, The Netherlands, 1956.
3. MackL. “Transition and Laminar Instability,” Jet Propulsion Lab., California Inst. of Technology JPL Publication 77-15, Pasadena, CA, 1977.
4. Correlation-Based Transition Modeling for Unstructured Parallelized Computational Fluid Dynamics Codes