Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study.

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

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)...

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Preliminary investigation of hollow-bladed turbines having closed and open blade tips /

Smith, Gordon T.
Hickel, Robert O.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"August 16, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Component performance investigation of J71 experimental turbine.

Petrash, Donald A.
Davison, Elmer H.
Schum, Harold J.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 2, 1956."Includes bibliographical references (p. 8).Mode of access: Internet

Design and experimental investigation of a high-weight-flow low-pressure-ratio turbine /

Petrash, Donald A.
Wasserbauer, Charles A.
Nunamaker, Robert R.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 14-15).Mode of access: Internet

Experimental investigation of partial- and full-admission characteristics of a two-stage velocity-compounded turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

A method for determining turbine design characteristics for rocket turbodrive applications /

Stewart, Warner L.
Whitney, Warren J.
Evans, David G.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 2, 1958."Includes bibliographical references (p. 23).Mode of access: Internet

Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives /

Wong, Robert Y.
Monroe Daniel E.
Darmstadt, David L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Design of turbine and experimental performance of first two stages /

Rohlik, Harold E.
Lewis Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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)...

Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor /

Graham, Robert W.
Prian, Vasily D.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"March 9, 1954."Includes bibliographical references (p. 10-11).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....

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

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)...

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Investigation of two-stage air-cooled turbine suitable for flight at mach number of 2.5.

Miser, James W.
Stewart, Warner L.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1956

"October 22, 1956."Includes bibliographical references (p. 17).Mode of access: Internet

Preliminary investigation of hollow-bladed turbines having closed and open blade tips /

Smith, Gordon T.
Hickel, Robert O.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"August 16, 1955."Includes bibliographical references (p. 10).Mode of access: Internet

Investigation of transonic turbine designed for zero diffusion of suction-surface velocity /

Whitney, Warren J.
Wong, Robert Y., joint author.
Monroe, Daniel E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "August 24, 1954."Title from cover.Includes bibliographical references: p. 9.Mode of...

Component performance investigation of J71 experimental turbine.

Petrash, Donald A.
Davison, Elmer H.
Schum, Harold J.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"October 2, 1956."Includes bibliographical references (p. 8).Mode of access: Internet

Design and experimental investigation of a high-weight-flow low-pressure-ratio turbine /

Petrash, Donald A.
Wasserbauer, Charles A.
Nunamaker, Robert R.
United States. National Aeronautics and Space Administration.

"September 1959."Cover title.Includes bibliographical reference (p. 14-15).Mode of access: Internet

Experimental investigation of partial- and full-admission characteristics of a two-stage velocity-compounded turbine /

Moffitt, Thomas P.
Klag, Frederick W.
Lewis Research Center.

January 1960

"October 1960."Cover title.Includes bibliographical references (p. 8).Mode of access: Internet

A method for determining turbine design characteristics for rocket turbodrive applications /

Stewart, Warner L.
Whitney, Warren J.
Evans, David G.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1958

"May 2, 1958."Includes bibliographical references (p. 23).Mode of access: Internet

Investigation of a 4.0-inch-mean-diameter four-stage reentry turbine for auxiliary power drives /

Wong, Robert Y.
Monroe Daniel E.
Darmstadt, David L.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1960

"March 1960."Cover title.Includes bibliographical references (p. 12-13).Mode of access: Internet

Design of turbine and experimental performance of first two stages /

Rohlik, Harold E.
Lewis Research Center.

January 1961

"May 1961."Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

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)...

Rotating stall investigation of the 0.72 hub-tip ratio single-stage compressor /

Graham, Robert W.
Prian, Vasily D.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"March 9, 1954."Includes bibliographical references (p. 10-11).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....

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

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)...

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study.

Abstract

Extracted data

Investigation of a 0.6 hub-tip radius-ratio transonic turbine designed for secondary-flow study.

Abstract

Extracted data

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