Add to ORKGStage-stacking technique for predicting over-all performance in multistage axial flow turbojet compressor using interstage-air blee
There is a common requirement in the process, oil and gas turbine industries for high performance ...
A complete stage of an axial-flow compressor designed to produce a high pressure ratio was investiga...
PART I: An analysis of a multi-stage axial compressor with high reaction blading is carried out...
Air was bled over the fifth-and tenth-stage rotor-blade rows through ports designed to pass 11 and 9...
The over-all performance of a 16-stage axial-flow compressor was determined with various stator-blad...
The compressor case of a 13-stage axial-flow compressor was modified to incorporate air-bleed system...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
A FORTRAN computer code is presented for off-design performance prediction of axial-flow compressors...
Multistage turbocompressor simulation applied to performance prediction of axial flow instabilitie
The 15-stage experimental axial-flow compressor was investigated at 78.5 percent of design speed, wh...
The performance of the first stage of a transonic, multistage compressor was mapped over a range of ...
A computer model of the J-85 gas turbine engine has been used in a investigation for potential ben...
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compresso
The design of modern gas-turbine engines is continuously being improved towards better performance, ...
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital ...
There is a common requirement in the process, oil and gas turbine industries for high performance ...
A complete stage of an axial-flow compressor designed to produce a high pressure ratio was investiga...
PART I: An analysis of a multi-stage axial compressor with high reaction blading is carried out...
Air was bled over the fifth-and tenth-stage rotor-blade rows through ports designed to pass 11 and 9...
The over-all performance of a 16-stage axial-flow compressor was determined with various stator-blad...
The compressor case of a 13-stage axial-flow compressor was modified to incorporate air-bleed system...
For use in computing the detailed performance parameters of individual blade rows of a multistage co...
A FORTRAN computer code is presented for off-design performance prediction of axial-flow compressors...
Multistage turbocompressor simulation applied to performance prediction of axial flow instabilitie
The 15-stage experimental axial-flow compressor was investigated at 78.5 percent of design speed, wh...
The performance of the first stage of a transonic, multistage compressor was mapped over a range of ...
A computer model of the J-85 gas turbine engine has been used in a investigation for potential ben...
Rotor design to evaluate outer case blowing or bleeding of single stage axial flow compresso
The design of modern gas-turbine engines is continuously being improved towards better performance, ...
A method of estimating the undistorted stall line for an axial-flow compressor by using the digital ...
There is a common requirement in the process, oil and gas turbine industries for high performance ...
A complete stage of an axial-flow compressor designed to produce a high pressure ratio was investiga...
PART I: An analysis of a multi-stage axial compressor with high reaction blading is carried out...