Add to ORKGA modified form of the Lam-Bremhorst low-Reynolds number kappa-epsilon turbulence model was developed for predicting transitional boundary layer flows under conditions characteristic of gas turbine blades. The application of the model to flows with pressure gradients is described. Tests against a number of turbine blade cascade data sets are included. Some additional refinements of the model that were made in recent months are explained
The development of high performance gas turbines requires high turbine inlet temperatures that can l...
Comparisons with experimental heat transfer and surface pressures were made for seven turbine vane a...
Reshotko has suggested that transition may be viewed as the response of a very complex three-dimensi...
A research effort was underway to study the use of two equation low Reynolds number turbulence model...
The use of low Reynolds number (LRN) forms of the k-epsilon turbulence model in predicting transitio...
The objective of the present research is to develop improved turbulence models for the computation o...
Turbine blade heat transfer is an important engineering problem characterized by complex flow fields...
Abstract. In turbomachines, transitional flows are likely to occur over many components. In the case ...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
The progress in modeling of transition on turbine vanes and blades performed under the sponsorship o...
The predictive qualities of a recently developed algebraic intermittency model for laminar-to-turbul...
Free-stream turbulence has an important effect on the local heat transfer coefficient around turbine...
AbstractThis article presents a linear eddy-viscosity turbulence model for predicting bypass and nat...
A symposium on transition in turbines was held at the NASA Lewis Research Center. One recommendation...
Improvement of the prediction of external (gas-to-blade) heat transfer coefficients in gas turbine e...
The development of high performance gas turbines requires high turbine inlet temperatures that can l...
Comparisons with experimental heat transfer and surface pressures were made for seven turbine vane a...
Reshotko has suggested that transition may be viewed as the response of a very complex three-dimensi...
A research effort was underway to study the use of two equation low Reynolds number turbulence model...
The use of low Reynolds number (LRN) forms of the k-epsilon turbulence model in predicting transitio...
The objective of the present research is to develop improved turbulence models for the computation o...
Turbine blade heat transfer is an important engineering problem characterized by complex flow fields...
Abstract. In turbomachines, transitional flows are likely to occur over many components. In the case ...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
The progress in modeling of transition on turbine vanes and blades performed under the sponsorship o...
The predictive qualities of a recently developed algebraic intermittency model for laminar-to-turbul...
Free-stream turbulence has an important effect on the local heat transfer coefficient around turbine...
AbstractThis article presents a linear eddy-viscosity turbulence model for predicting bypass and nat...
A symposium on transition in turbines was held at the NASA Lewis Research Center. One recommendation...
Improvement of the prediction of external (gas-to-blade) heat transfer coefficients in gas turbine e...
The development of high performance gas turbines requires high turbine inlet temperatures that can l...
Comparisons with experimental heat transfer and surface pressures were made for seven turbine vane a...
Reshotko has suggested that transition may be viewed as the response of a very complex three-dimensi...