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

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

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.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 two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).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

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

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

Rohlik, Harold E.
Scibbe, Herbert W.
Wintucky, William T.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1957

"January 9, 1957."Includes bibliographical references (p. 13-14).Mode of access: Internet

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

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

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).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 an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F /

Cochran, Reeves P.
Dengler, Robert P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Propulsion system elements; Propulsion systems, air-jet.Includes bibliograph...

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)...

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

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 /

Nugent, Jack.
Powers, Bruce G.
United States. National Aeronautics and Space Administration.

"September 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

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

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.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 two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).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

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

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

Rohlik, Harold E.
Scibbe, Herbert W.
Wintucky, William T.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1957

"January 9, 1957."Includes bibliographical references (p. 13-14).Mode of access: Internet

Experimental investigation of the partial- admission performance characteristics of a single-stage Mach 2 supersonic turbine /

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

January 1959

"September 1959."Cover title.Includes bibliographical references (p. 8).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 an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F /

Cochran, Reeves P.
Dengler, Robert P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Propulsion system elements; Propulsion systems, air-jet.Includes bibliograph...

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)...

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

Considerations of turbine cooling systems for Mach 3 flight /

Stepka, Francis S.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."April 1968."Includes bibliographical references (p. 32).Mode of access: Internet

Flight tests of a twin-duct induction system for a mach number range of 0.78 to 2.07 /

Nugent, Jack.
Powers, Bruce G.
United States. National Aeronautics and Space Administration.

"September 1960."Cover title.Includes bibliographical references (p. 14).Mode of access: Internet

Investigations of air-cooled turbine rotors for turbojet engines

Nachtigall, Alfred J.
Ziemer, Robert R., joint author.
Zalabak, Charles F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 21, 1952."Title from cover.Includes bibliographical references: p. 22.Mode of a...

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

Altitude-wind-tunnel investigation of a 4000-pound-thrust axial-flow turbojet engine

Fleming, William A.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 3, 1948."Includes bibliographical references: p. 17.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

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

Abstract

Extracted data

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

Abstract

Extracted data

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