Experimental performance of a 5-inch single-stage axial-flow turbine designed for a Brayton cycle space power system

Experimental performance evaluation of a 6.02-inch radial-inflow turbine over a range of Reynolds number

Holeski, D. E.
Futral, S. M., Jr.

January 1967

Experimental performance evaluation of radial inflow turbine over range of inlet total pressur

Design and Experimental Investigation of a High-weight-flow Low-pressure-ratio Turbine

Petrash, D. A.
Nunamaker, R. R.
Wasserbauer, C. A.

September 1959

Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...

Experimental performance evaluation of an 8.5 inch /21.59 cm/ mean-diameter axial flow turbine at Reynolds numbers from 18,000 to 177,000

Kofskey, M. G.
Nusbaum, W. J.

March 1968

Effects of Reynolds number change on performance of axial flow turbine working in argo

Experimental performance of a 5-inch /13 cm/ axial-flow turbine over a range of Reynolds number

Futral, S. M., Jr.
Holeski, D. E.

October 1968

Efficiency, mass flow rate, torque, and exit diffuser effectiveness of 5-inch axial flow turbin

Cold performance evaluation of a 4.59-inch radial-inflow turbine designed for a Brayton- cycle space power system

Wasserbauer, C. A.
Nusbaum, W. J.
Kofskey, M. G.

February 1966

Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...

Overall performance in argon of a 3.7-inch six-stage axial-flow compressor

Tysl, E. R.
Weigel, C., Jr.
Heidelberg, L. J.

March 1971

Performance of axial flow compressor for Brayton cycle electrical power generating system with argo

Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine. 1: Design and performance of a solid blade configuration

Haas, J. E.
Kofskey, M. G.

January 1975

A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...

Cold performance evaluation of a 6.02-inch radial inflow turbine designed for a 10-kilowatt shaft output Brayton cycle space power generation system

Holeski, D. E.
Kofskey, M. G.

February 1966

Cold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft out...

Turbine for ordnance turbojet engine. 2: Cold-air performance with opened stator

Nusbaum, W. J.
Kofskey, M. G.
Haas, J. E.

June 1974

A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...

Effect of axial running clearance on performance of two Brayton cycle radial inflow turbines

Nusbaum, W. J.
Futral, S. M., Jr.

February 1969

Axial running clearance effect on efficiency and mass flow rate of Brayton cycle radial inflow turbi...

The aerodynamic design of a compressor-drive turbine for use in a 75 kw automotive engine

Mclallin, K. L.
Roelke, R. J.

April 1975

The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...

Performance evaluation of a two stage axial-flow turbine for two values of tip clearance

Kofskey, M. G.
Nusbaum, W. J.

January 1968

Performance of two-stage axial flow turbine operating at different rotor tip clearanc

Turbine and compressor performance of a Brayton rotating unit during hot closed-loop operation

Wong, R. Y.
Klassen, H. A.
Evans, R. C.

September 1971

Efficiency estimates of turbine and compressor components of Brayton rotating unit during hot closed...

Turbine research package for research and development of high performance turboalternator Final report

Cohen, R.
Havens, F. D.
Gilroy, W. K.

January 1967

Two-stage, axial flow turbine test rig for providing cold flow aerodynamic performance data on Brayt...

Preliminary performance of a 4.97-inch radial turbine operating in a Brayton power system with a helium-xenon gas mixture

Curreri, J. S.
Ream, L. W.
Leroy, M. J., Jr.

December 1971

The performance characteristics of the Brayton-rotating-unit's 4.97-inch radial turbine were investi...

Experimental performance evaluation of a 6.02-inch radial-inflow turbine over a range of Reynolds number

Holeski, D. E.
Futral, S. M., Jr.

January 1967

Experimental performance evaluation of radial inflow turbine over range of inlet total pressur

Design and Experimental Investigation of a High-weight-flow Low-pressure-ratio Turbine

Petrash, D. A.
Nunamaker, R. R.
Wasserbauer, C. A.

September 1959

Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...

Experimental performance evaluation of an 8.5 inch /21.59 cm/ mean-diameter axial flow turbine at Reynolds numbers from 18,000 to 177,000

Kofskey, M. G.
Nusbaum, W. J.

March 1968

Effects of Reynolds number change on performance of axial flow turbine working in argo

Experimental performance of a 5-inch /13 cm/ axial-flow turbine over a range of Reynolds number

Futral, S. M., Jr.
Holeski, D. E.

October 1968

Efficiency, mass flow rate, torque, and exit diffuser effectiveness of 5-inch axial flow turbin

Cold performance evaluation of a 4.59-inch radial-inflow turbine designed for a Brayton- cycle space power system

Wasserbauer, C. A.
Nusbaum, W. J.
Kofskey, M. G.

February 1966

Cold performance characteristics of small radial inflow turbine designed for Brayton cycle power sys...

Overall performance in argon of a 3.7-inch six-stage axial-flow compressor

Tysl, E. R.
Weigel, C., Jr.
Heidelberg, L. J.

March 1971

Performance of axial flow compressor for Brayton cycle electrical power generating system with argo

Cold-air performance of a 12.766-centimeter-tip-diameter axial-flow cooled turbine. 1: Design and performance of a solid blade configuration

Haas, J. E.
Kofskey, M. G.

January 1975

A solid blade version of a single-stage, axial-flow turbine was investigated to determine its perfor...

Cold performance evaluation of a 6.02-inch radial inflow turbine designed for a 10-kilowatt shaft output Brayton cycle space power generation system

Holeski, D. E.
Kofskey, M. G.

February 1966

Cold argon and air performance of 6.02 inch radial inflow turbine designed for 10 kilowatt shaft out...

Turbine for ordnance turbojet engine. 2: Cold-air performance with opened stator

Nusbaum, W. J.
Kofskey, M. G.
Haas, J. E.

June 1974

A single-stage axial-flow turbine was investigated to determine the effect of increased stator throa...

Effect of axial running clearance on performance of two Brayton cycle radial inflow turbines

Nusbaum, W. J.
Futral, S. M., Jr.

February 1969

Axial running clearance effect on efficiency and mass flow rate of Brayton cycle radial inflow turbi...

The aerodynamic design of a compressor-drive turbine for use in a 75 kw automotive engine

Mclallin, K. L.
Roelke, R. J.

April 1975

The design of a single stage axial-flow turbine with a tip diameter of 11.15 cm is presented. The de...

Performance evaluation of a two stage axial-flow turbine for two values of tip clearance

Kofskey, M. G.
Nusbaum, W. J.

January 1968

Performance of two-stage axial flow turbine operating at different rotor tip clearanc

Turbine and compressor performance of a Brayton rotating unit during hot closed-loop operation

Wong, R. Y.
Klassen, H. A.
Evans, R. C.

September 1971

Efficiency estimates of turbine and compressor components of Brayton rotating unit during hot closed...

Turbine research package for research and development of high performance turboalternator Final report

Cohen, R.
Havens, F. D.
Gilroy, W. K.

January 1967

Two-stage, axial flow turbine test rig for providing cold flow aerodynamic performance data on Brayt...

Preliminary performance of a 4.97-inch radial turbine operating in a Brayton power system with a helium-xenon gas mixture

Curreri, J. S.
Ream, L. W.
Leroy, M. J., Jr.

December 1971

The performance characteristics of the Brayton-rotating-unit's 4.97-inch radial turbine were investi...

Experimental performance evaluation of a 6.02-inch radial-inflow turbine over a range of Reynolds number

Holeski, D. E.
Futral, S. M., Jr.

January 1967

Experimental performance evaluation of radial inflow turbine over range of inlet total pressur

Design and Experimental Investigation of a High-weight-flow Low-pressure-ratio Turbine

Petrash, D. A.
Nunamaker, R. R.
Wasserbauer, C. A.

September 1959

Performance characteristics of high-weight flow, low pressure ratio, single stage turbine rotor and ...

Experimental performance evaluation of an 8.5 inch /21.59 cm/ mean-diameter axial flow turbine at Reynolds numbers from 18,000 to 177,000

Kofskey, M. G.
Nusbaum, W. J.

March 1968

Effects of Reynolds number change on performance of axial flow turbine working in argo

Experimental performance of a 5-inch single-stage axial-flow turbine designed for a Brayton cycle space power system

Abstract

Extracted data

Experimental performance of a 5-inch single-stage axial-flow turbine designed for a Brayton cycle space power system

Abstract

Extracted data

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