Add to ORKGThis paper describes measurements of the performance of a research stage operating in isolation and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
A low-order unsteady one-dimensional axial compressor and combustor model has been developed at Cran...
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital ...
For most compressor flows, the existence of turbulent shear stresses is essential to compensate and ...
\Yith the current develop111ent in computer technology and Computational Fluid D)"n<'tlllics techni...
Stage-stacking technique for predicting over-all performance in multistage axial flow turbojet compr...
Four separate tasks are reported. The first task: A Computational Model for Short Wavelength Stall I...
A FORTRAN computer code is presented for off-design performance prediction of axial-flow compressors...
The design of modern gas-turbine engines is continuously being improved towards better performance, ...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
Purpose – This paper aims to validate and analyse the NASA35 axial compressor performance base...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
A computer model of the J-85 gas turbine engine has been used in a investigation for potential ben...
The objective of the work described in this thesis is twofold; to elucidate the nature of stall and...
This paper describes measurements of the performance of a research stage operating in isolation and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
A low-order unsteady one-dimensional axial compressor and combustor model has been developed at Cran...
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital ...
For most compressor flows, the existence of turbulent shear stresses is essential to compensate and ...
\Yith the current develop111ent in computer technology and Computational Fluid D)"n<'tlllics techni...
Stage-stacking technique for predicting over-all performance in multistage axial flow turbojet compr...
Four separate tasks are reported. The first task: A Computational Model for Short Wavelength Stall I...
A FORTRAN computer code is presented for off-design performance prediction of axial-flow compressors...
The design of modern gas-turbine engines is continuously being improved towards better performance, ...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform m...
Purpose – This paper aims to validate and analyse the NASA35 axial compressor performance base...
A three dimensional unsteady Reynolds-Averaged Navier-Stokes solver was used to perform multistage u...
A computer model of the J-85 gas turbine engine has been used in a investigation for potential ben...
The objective of the work described in this thesis is twofold; to elucidate the nature of stall and...
This paper describes measurements of the performance of a research stage operating in isolation and ...
Thesis (M.S.)--Massachusetts Institute of Technology, Dept. of Aeronautics and Astronautics, 1998.In...
A low-order unsteady one-dimensional axial compressor and combustor model has been developed at Cran...