Significant progress was made in advancing the idea of establishing a unified approach for predicting airfoil heat transfer for a wide range of operating conditions and geometries. Preliminary results are encouraging and further mixing length (ml) turbulence modeling ideas will be explored, concentrating on transition behavior. The capability of available modeling techniques to predict airfoil surface heat transfer distributions in a two-dimensional flow field was assessed, experimental data as required for model verification were acquired, and improvements in the analytic models was made and verified
The effect of secondary flows on mass transfer from a simulated gas turbine blade and hubwall is inv...
Emphasis is placed on developing more accurate analytical models for predicting turbine airfoil exte...
Predictions of turbine vane and endwall heat transfer and pressure distributions are compared with e...
Improvements in methods for predicting heat transfer rates on the hot gas side of turbine airfoils a...
Three airfoil data sets were selected for use in evaluating currently available analytical models fo...
The primary basis for heat transfer analysis of turbine airfoils is experimental data obtained in li...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
Improvement of the prediction of external (gas-to-blade) heat transfer coefficients in gas turbine e...
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...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The taxonomy of flow phenomena affecting turbine blade heat transfer has been widely researched and ...
The effect of secondary flows on mass transfer from a simulated gas turbine blade and hubwall is inv...
Detailed heat transfer measurements and predictions are given for a power generation turbine rotor w...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
The effect of secondary flows on mass transfer from a simulated gas turbine blade and hubwall is inv...
Emphasis is placed on developing more accurate analytical models for predicting turbine airfoil exte...
Predictions of turbine vane and endwall heat transfer and pressure distributions are compared with e...
Improvements in methods for predicting heat transfer rates on the hot gas side of turbine airfoils a...
Three airfoil data sets were selected for use in evaluating currently available analytical models fo...
The primary basis for heat transfer analysis of turbine airfoils is experimental data obtained in li...
A program sponsored by NASA for the investigation of the heat transfer in the transition region of t...
Improvement of the prediction of external (gas-to-blade) heat transfer coefficients in gas turbine e...
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...
Due to the character of the original source materials and the nature of batch digitization, quality ...
The taxonomy of flow phenomena affecting turbine blade heat transfer has been widely researched and ...
The effect of secondary flows on mass transfer from a simulated gas turbine blade and hubwall is inv...
Detailed heat transfer measurements and predictions are given for a power generation turbine rotor w...
In current and advanced gas turbine engines, increased speeds, pressures and temperatures are used t...
The effect of secondary flows on mass transfer from a simulated gas turbine blade and hubwall is inv...
Emphasis is placed on developing more accurate analytical models for predicting turbine airfoil exte...
Predictions of turbine vane and endwall heat transfer and pressure distributions are compared with e...