Performance in air of 4-inch- (10.16-cm- ) mean-diameter single-stage axial-flow turbine for Reynolds numbers from 4900 to 188,000 /

Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading /

McLallin, Kerry L.
Haas, Jeffrey E.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Propulsion Laboratory.""Lewis Research Center."Includes bibliographical references.Mode o...

Experimental investigation of a 3.0-inch-mean-diameter full-admission three-stage turbine suitable for small auxiliary power units /

Wong, Robert Y. (Robert Young)
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1965"--Cover.Includes bibliographical references (p. 21)...

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system /

Kofskey, Milton G.
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 28)...

Air-performance evaluation of a 4.0-inch-mean-diameter single-stage turbine at various inlet pressures from 0.14 to 1.88 atmospheres and corresponding Reynolds numbers from 2500 to 50,000 /

Wong, Robert Y.
Nusbaum, William J.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Power sources, supplementary; Propulsion systems, air-jet.Includes bibliog...

Experimental performance evaluation of an 8.5-inch- (21.59-cm-) mean-diameter axial-flow trubine at reynolds numbers from 18 000 to 177 000 /

Nusbaum, William J.
Kofskey, Milton G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 20).Mode of access: Internet

Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance /

Whitney, Warren J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Inter...

Cold-air performance of a 15.41-cm-tip-diameter axial-flow power turbine with variable-area stator designed for a 75-kW automotive gas turbine engine /

McLallin, Kerry L.
Wong, Robert Y.
Kofskey, Milton G.
United States. Dept. of Energy. Office of Vehicle and Engine Research and Development.
Lewis Research Center.

January 1982

Prepared at Lewis Research Center."Work performed for U.S. Department of Energy, Conservation and Re...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 /

Whitney, Warren J.
Behning, Frank P.
Moffitt, Thomas P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Jan. 1981."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Experimental results of varying the blade-shroud clearance in a 6.02-inch radial-inflow turbine /

Futral, Samuel M.
Holeski, Donald E.

Prepared at Lewis Research Center."January 1970."Cover title.Includes bibliographical references (p....

Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 /

Osborn, Walter Martin, 1918-
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ac...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage /

Moore, Royce D.
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Bibliography: p. 19.Mode of access: Int...

Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading /

McLallin, Kerry L.
Haas, Jeffrey E.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Propulsion Laboratory.""Lewis Research Center."Includes bibliographical references.Mode o...

Experimental investigation of a 3.0-inch-mean-diameter full-admission three-stage turbine suitable for small auxiliary power units /

Wong, Robert Y. (Robert Young)
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1965"--Cover.Includes bibliographical references (p. 21)...

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Aerodynamic evaluation of two-stage axial-flow turbine designed for Brayton-cycle space power system /

Kofskey, Milton G.
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1968"--Cover.Includes bibliographical references (p. 28)...

Air-performance evaluation of a 4.0-inch-mean-diameter single-stage turbine at various inlet pressures from 0.14 to 1.88 atmospheres and corresponding Reynolds numbers from 2500 to 50,000 /

Wong, Robert Y.
Nusbaum, William J.
United States. National Aeronautics and Space Administration.

Cover title."August 1962."Power sources, supplementary; Propulsion systems, air-jet.Includes bibliog...

Experimental performance evaluation of an 8.5-inch- (21.59-cm-) mean-diameter axial-flow trubine at reynolds numbers from 18 000 to 177 000 /

Nusbaum, William J.
Kofskey, Milton G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."March 1968."Includes bibliographical references (p. 20).Mode of access: Internet

Cold-air investigation of 4 1/2-stage turbine with stage-loading factor of 4.66 and high specific work output : II - stage group performance /

Whitney, Warren J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1980

"June 1980"--Cover."Lewis Research Center."Includes bibliographical references.Mode of access: Inter...

Cold-air performance of a 15.41-cm-tip-diameter axial-flow power turbine with variable-area stator designed for a 75-kW automotive gas turbine engine /

McLallin, Kerry L.
Wong, Robert Y.
Kofskey, Milton G.
United States. Dept. of Energy. Office of Vehicle and Engine Research and Development.
Lewis Research Center.

January 1982

Prepared at Lewis Research Center."Work performed for U.S. Department of Energy, Conservation and Re...

Performance of centerbody vortex generators in an axisymmetric mixed-compression inlet at Mach numbers from 2.0 to 3.0 /

Mitchell, Glen A.
Davis, Ronald W.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 12).Mode of access: Internet

Stalled and stall-free performance of axial-flow compressor stage with three inlet-guide-vane and stator-blade settings /

Urasek, Donald C.
Cunnan, Walter S.
Steinke, Ronald J.
Lewis Research Center.

January 1977

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 13).Mode of ac...

Cold-air investigation of first state of 4 1/2-stage, fan-drive turbine with average stage-loading factor of 4.66 /

Whitney, Warren J.
Behning, Frank P.
Moffitt, Thomas P.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

Jan. 1981."Lewis Research Center."Includes bibliographical references.Mode of access: Internet

Experimental results of varying the blade-shroud clearance in a 6.02-inch radial-inflow turbine /

Futral, Samuel M.
Holeski, Donald E.

Prepared at Lewis Research Center."January 1970."Cover title.Includes bibliographical references (p....

Performance of a 1.15-pressure-ratio axial-flow fan stage with a blade tip solidity of 0.5 /

Osborn, Walter Martin, 1918-
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 20).Mode of ac...

Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 /

Moore, Royce D.
Reid, Lonnie.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

STAR category 07."Lewis Research Center.""February 1982"--Cover.Includes bibliographical references....

Aerodynamic performance of a 1.25-pressure-ratio axial-flow fan stage /

Moore, Royce D.
Steinke, Ronald J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Chiefly tables.Cover title.Bibliography: p. 19.Mode of access: Int...

Experimental performance and analysis of 15.04-centimeter-tip-diameter, radial-inflow turbine with work factor of 1.126 and thick blading /

McLallin, Kerry L.
Haas, Jeffrey E.
Propulsion Laboratory (U.S.)
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Oct. 1980."Propulsion Laboratory.""Lewis Research Center."Includes bibliographical references.Mode o...

Experimental investigation of a 3.0-inch-mean-diameter full-admission three-stage turbine suitable for small auxiliary power units /

Wong, Robert Y. (Robert Young)
Nusbaum, William J.
Lewis Research Center.

Prepared at Lewis Research Center."February 1965"--Cover.Includes bibliographical references (p. 21)...

Aerodynamic performance of axial-flow fan stage operated at nine inlet guide vane angles /

Moore, Royce D.
Reid, Lonnie.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1979

"September 1979"--Cover.Includes bibliographical references (p. 12).Mode of access: Internet

Performance in air of 4-inch- (10.16-cm- ) mean-diameter single-stage axial-flow turbine for Reynolds numbers from 4900 to 188,000 /

Abstract

Extracted data

Performance in air of 4-inch- (10.16-cm- ) mean-diameter single-stage axial-flow turbine for Reynolds numbers from 4900 to 188,000 /

Abstract

Extracted data

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