With the interest in jet propulsion at the end of World War II, aerodynamicists were challenged to develop mathematical models which could be used to design turbomachinery components for jets. NASA Lewis engineers and scientists played a major role in meeting this challenge. Some of their accomplishments are highlighted as well as those of others. Several problems are addressed which must be solved if jet propulsion technology is to advance
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The following dissertation examines several aspects of numerical simulations for turbomachinery flow...
The design of a two-stream wind tunnel was undertaken to allow the simulation and study of certain ...
Significant advancements have been made in the last five years in the ability to model turbomachiner...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
This Wu Chang-Hua lecture is concerned with the development of analysis and computational capability...
A computational model was developed at the NASA Glenn Research Center to investigate possible uses o...
PaperPg. 123-150.Any performance gain in a turbomachinery system requires some advancements in a num...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
Turbomachinery system components and associated technologies are discussed. Specific technologies re...
The use of computerized simulations of the steady state and transient performance of jet engines thr...
The results of a numerical simulation of the time-averaged inviscid flow field through the blade row...
The design practices for the gas turbine are traced throughout history with particular emphasis on t...
An unsteady, multiblock, Reynolds Averaged Navier Stokes solver based on Runge-Kutta scheme and Pseu...
The following dissertation examines several aspects of numerical simulations for turbomachinery flow...
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The following dissertation examines several aspects of numerical simulations for turbomachinery flow...
The design of a two-stream wind tunnel was undertaken to allow the simulation and study of certain ...
Significant advancements have been made in the last five years in the ability to model turbomachiner...
Computer program calculates the velocity distribution and streamlines over widely separated blades o...
This Wu Chang-Hua lecture is concerned with the development of analysis and computational capability...
A computational model was developed at the NASA Glenn Research Center to investigate possible uses o...
PaperPg. 123-150.Any performance gain in a turbomachinery system requires some advancements in a num...
The development of a design/analysis flow solver at NASA Lewis Research Center is discussed. The sol...
Turbomachinery system components and associated technologies are discussed. Specific technologies re...
The use of computerized simulations of the steady state and transient performance of jet engines thr...
The results of a numerical simulation of the time-averaged inviscid flow field through the blade row...
The design practices for the gas turbine are traced throughout history with particular emphasis on t...
An unsteady, multiblock, Reynolds Averaged Navier Stokes solver based on Runge-Kutta scheme and Pseu...
The following dissertation examines several aspects of numerical simulations for turbomachinery flow...
Research to develop high-speed airbreathing aerospace propulsion systems was underway in the late 19...
The following dissertation examines several aspects of numerical simulations for turbomachinery flow...
The design of a two-stream wind tunnel was undertaken to allow the simulation and study of certain ...