An investigation of the flow characteristics in the blade endwall corner region /

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Murthy, A. V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

Flow through a wire-form transpiration-cooled vane /

Kaufman, Albert, 1928-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 15.Mode of access: Internet

An experimental study of near wall flow parameters in the blade end-wall corner region /

Bhargava, Rakesh K.
Raj, Rishi S.
Lewis Research Center.

January 1989

"Prepared for Lewis Research Center under Grant NAG3-122."Bibliography: p. 282-297.Mode of access: I...

Flow measurement in base cooling air passages of a rotating turbine blade /

Liebert, Curt H.
Pollack, Frank G.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Visualization of secondary-flow phenomena in blade row /

Herzig, H. Z.
Costello, G. R., joint author.
Hansen, A. G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 26, 1952."Title from cover.Includes bibliographical references: p. 8.Mode of...

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....

Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine /

Haas, Jeffrey E.
Boyle, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 07."September 1984"--Cover.Distributed to depository libraries in microfiche.Includes ...

Analysis of internal flow characteristics of a smooth-disk water-brake dynamometer /

Evans, David G.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 39.Mode of access: Internet

Flow through very porous screens /

Durbin, Paul A.
Muramoto, Kenneth Kenichiro.
Lewis Research Center.

January 1985

Prepared at Lewis Research Center."March 1985"--Cover.Includes bibliographical references (p. 10).Mo...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

End wall flow characteristics and overall performance of an axial flow compressor stage /

Sitaram, N.
Lakshminarayana, B.
Pennsylvania State University.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

"February 1983"--Cover."Pennsylvania State University."Includes bibliographical references.Mode of a...

A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine blade /

Katsanis, Theodore.
Dellner, Lois T.
Lewis Research Center.

January 1967

"NASA TM X-1394.""Lewis Research Center, Cleveland, Ohio.""June 1967"--Cover.Includes bibliographica...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Murthy, A. V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

Flow through a wire-form transpiration-cooled vane /

Kaufman, Albert, 1928-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 15.Mode of access: Internet

An experimental study of near wall flow parameters in the blade end-wall corner region /

Bhargava, Rakesh K.
Raj, Rishi S.
Lewis Research Center.

January 1989

"Prepared for Lewis Research Center under Grant NAG3-122."Bibliography: p. 282-297.Mode of access: I...

Flow measurement in base cooling air passages of a rotating turbine blade /

Liebert, Curt H.
Pollack, Frank G.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Computer analysis of flow pertubations generated by placement of choke bumps in a wind tunnel /

Campbell, Richard L. (Richard Lawson), 1952-
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1981

"August 1981"--Cover."Langley Research Center."Includes bibliographical references.Mode of access: I...

Visualization of secondary-flow phenomena in blade row /

Herzig, H. Z.
Costello, G. R., joint author.
Hansen, A. G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 26, 1952."Title from cover.Includes bibliographical references: p. 8.Mode of...

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....

Analytical and experimental investigation of stator endwall contouring in a small axial-flow turbine /

Haas, Jeffrey E.
Boyle, Robert J.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

STAR category 07."September 1984"--Cover.Distributed to depository libraries in microfiche.Includes ...

Analysis of internal flow characteristics of a smooth-disk water-brake dynamometer /

Evans, David G.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 39.Mode of access: Internet

Flow through very porous screens /

Durbin, Paul A.
Muramoto, Kenneth Kenichiro.
Lewis Research Center.

January 1985

Prepared at Lewis Research Center."March 1985"--Cover.Includes bibliographical references (p. 10).Mo...

Experimental and analytical study of a conically diffused flow with a nearly separated boundary layer /

Boldman, Donald R.
Neumann, Harvey E.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 38-39).Mode of...

End wall flow characteristics and overall performance of an axial flow compressor stage /

Sitaram, N.
Lakshminarayana, B.
Pennsylvania State University.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

"February 1983"--Cover."Pennsylvania State University."Includes bibliographical references.Mode of a...

A quasi-three-dimensional method for calculating blade surface velocities for an axial flow turbine blade /

Katsanis, Theodore.
Dellner, Lois T.
Lewis Research Center.

January 1967

"NASA TM X-1394.""Lewis Research Center, Cleveland, Ohio.""June 1967"--Cover.Includes bibliographica...

Evaluation of flow quality in two large NASA wind tunnels at transonic speeds /

Harvey, Bill.
Owen, F. Kevin.
Stainback, P. Calvin.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1980

Subject Category 34."December 1980"--Cover."Langley Research Center."Includes bibliographical refere...

Aerofoil testing in a self-streamlining flexible walled wind tunnel /

Lewis, Mark Charles.
Langley Research Center.

January 1988

"May 1988"--Cover."Prepared for Langley Research Center under Grant NSG-7172."Includes bibliographic...

Studies of sidewall boundary layer in the Langley 0.3-Meter Transonic Cryogenic Tunnel with and without suction /

Murthy, A. V.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1983

Subject category 34."Langley Research Center.""March 1983"--Cover.Includes bibliographical reference...

Flow through a wire-form transpiration-cooled vane /

Kaufman, Albert, 1928-
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Bibliography: p. 15.Mode of access: Internet

An investigation of the flow characteristics in the blade endwall corner region /

Abstract

Extracted data

An investigation of the flow characteristics in the blade endwall corner region /

Abstract

Extracted data

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