The development of a unified one-equation model for the prediction of trans
itional and turbulent flows is described herein. An eddy-viscosity-transpor
t equation for nonturbulent fluctuation growth based on that proposed by Wa
rren and Hassan (Warren, E. S., and Hassan, H. A., "Transition Closure Mode
l for Predicting Transition Onset ' "Journal of Aircraft, Vol. 35, No. 5,19
98, pp. 769-775) is combined with the Spalart-Allmaras one-equation model f
or turbulent fluctuation growth. Blending of the two equations is accomplis
hed through a multidimensional intermittency function based on the work of
Dhawan and Narasimha (Dhawan, S., and Narashima, R., "Some Properties of Bo
undary Layer Flow During Transition from Laminar to Turbulent Motion," Jour
nal of Fluid Mechanics, Vol. 3, No. 4, 1958, pp. 418-436). The model predic
ts both the onset and extent of transition. Low-speed test cases include tr
ansitional flow over a flat plate, a single-element airfoil, a multielement
airfoil in landing configuration, and a circular cylinder. Simulations of
Mach 3.5 transitional flow over a 5-deg cone are also presented. Results ar
e compared with experimental data, and the spatial accuracy of selected pre
dictions is analyzed.