Incidence loss for a core turbine rotor blade in a two-dimensional cascade /

Turbine blade wear by coal ash in working fluid at 1,200⁰F /

Goff, Gerald B.
Strimbeck, Donald C.
Liberatore, Arthur J.
McGee, J. P.
McGee, James P.
United States. Bureau of Mines.

"April 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

Incidence loss for fan turbine rotor blade in two-dimensional cascade /

Kline, John F.
Stabe, Roy G.
Moffitt, Thomas P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."July 1983"--Cover.Distributed to depository libraries in microfiche."Lewis Researc...

Effects of increased leading-edge thickness on performance of a transonic rotor blade /

Reid, Lonnie.
Urasek, Donald C.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade /

Stabe, Roy G.
Liebert, Curt H.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8).Mode of acc...

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...

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....

Research turbine for high-temperature core engine application /

Szanca, Edward M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Cold-air overal...

Pressure-loss and flow coefficients inside a chordwise-finned, impingement, convection, and film air-cooled turbine vane /

Hippensteele, Steven A.
Lewis Research Center.

January 1974

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

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

An adverse effect of film cooling on the suction surface of a turbine vane /

Gladden, Herbert J.
Gauntner, James W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

Computer program for design analysis of radial-inflow turbines /

Glassman, Arthur J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 58).Mode of ac...

Miniature sheathed thermocouples for turbine blade temperature measurement /

Holanda, Raymond.
Krause, Lloyd N.
Glawe, George E.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

A cascade investigation of a convection- and film-cooled turbine vane made from radially stacked laminates /

Gladden, Herbert J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode of...

Turbine blade wear by coal ash in working fluid at 1,200⁰F /

Goff, Gerald B.
Strimbeck, Donald C.
Liberatore, Arthur J.
McGee, J. P.
McGee, James P.
United States. Bureau of Mines.

"April 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

Incidence loss for fan turbine rotor blade in two-dimensional cascade /

Kline, John F.
Stabe, Roy G.
Moffitt, Thomas P.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Lewis Research Center.

January 1983

STAR category 07."July 1983"--Cover.Distributed to depository libraries in microfiche."Lewis Researc...

Effects of increased leading-edge thickness on performance of a transonic rotor blade /

Reid, Lonnie.
Urasek, Donald C.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 19).Mode of ac...

Aerodynamic performance of a ceramic-coated core turbine vane tested with cold air in a two-dimensional cascade /

Stabe, Roy G.
Liebert, Curt H.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8).Mode of acc...

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...

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....

Research turbine for high-temperature core engine application /

Szanca, Edward M.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references.1. Cold-air overal...

Pressure-loss and flow coefficients inside a chordwise-finned, impingement, convection, and film air-cooled turbine vane /

Hippensteele, Steven A.
Lewis Research Center.

January 1974

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

Dispersion of turbojet engine exhaust in flight /

Holdeman, James D.
Lewis Research Center.

January 1973

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ac...

An adverse effect of film cooling on the suction surface of a turbine vane /

Gladden, Herbert J.
Gauntner, James W.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

Computer program for design analysis of radial-inflow turbines /

Glassman, Arthur J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 58).Mode of ac...

Miniature sheathed thermocouples for turbine blade temperature measurement /

Holanda, Raymond.
Krause, Lloyd N.
Glawe, George E.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 12-13).Mode of...

A cascade investigation of a convection- and film-cooled turbine vane made from radially stacked laminates /

Gladden, Herbert J.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode of...

Turbine blade wear by coal ash in working fluid at 1,200⁰F /

Goff, Gerald B.
Strimbeck, Donald C.
Liberatore, Arthur J.
McGee, J. P.
McGee, James P.
United States. Bureau of Mines.

"April 1969"--Cover.Includes bibliographical references.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

Incidence loss for a core turbine rotor blade in a two-dimensional cascade /

Abstract

Extracted data

Incidence loss for a core turbine rotor blade in a two-dimensional cascade /

Abstract

Extracted data

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