Effect of high rotor pressure-surface diffusion on performance of a transonic turbine /

Performance comparisons of high mach number compressor rotor blading /

Gostelow, J. P.
Smith, L. H.
Krabacher, K. W.
Lewis Research Center.
General Electric Company.
United States. National Aeronautics and Space Administration.

January 1968

"December 1968."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

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...

Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall /

Hanson, Morgan P.
Meyer, Andre J.
Johnson, Donald F.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"June 13 1955."Includes bibliographical references (p. 7-8).Mode of access: Internet

Effect of a reduction in stator solidity on performance of a transonic turbine /

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

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

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...

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor /

Schacht, Ralph L.
Goldstein, Arthur W.
Cullom, Richard R.
Lewis Research Center.

January 1959

"October 1959."Caption title.Includes bibliographical references (p. 16-17).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

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

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 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

Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /

Cochran, Reeves P.
Dengler, Robert P.
Cochran, Reeves P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 15, 1955."Cover title.Includes bibliographical references (p...

Effect of pressure ratio and inlet pressure on performance of experimental gas turbine at inlet temperature of 800©� R /

Kohl, Robert C.
Larkin, Robert G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 2, 1948."Includes bibliographical references: p. 4.Mode of access: Interne...

Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine /

Dunbar, William R.
Hurrell, Herbert G.
Vasu, George.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 20, 1955."Includes bibliographical references (p. 24).Mode of access: Internet

Performance of compressor blade cascades at high Mach numbers /

Bogdonoff, Seymour M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"June 12, 1947."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Performance comparisons of high mach number compressor rotor blading /

Gostelow, J. P.
Smith, L. H.
Krabacher, K. W.
Lewis Research Center.
General Electric Company.
United States. National Aeronautics and Space Administration.

January 1968

"December 1968."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

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...

Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall /

Hanson, Morgan P.
Meyer, Andre J.
Johnson, Donald F.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"June 13 1955."Includes bibliographical references (p. 7-8).Mode of access: Internet

Effect of a reduction in stator solidity on performance of a transonic turbine /

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

"Declassified December 3, 1958.""March 23, 1956."Cover title.Includes bibliographical references (p....

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...

Investigation of the performance of a turbojet engine with variable-position compressor inlet guide vanes /

Budinger, Ray E.
Kaufman, Harold R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"October 4, 1955."Includes bibliographical references (p. 20).Mode of access: Internet

Performance of a straight stator and a tilted stator tested with a high-solidity high-pressure-ratio transonic rotor /

Schacht, Ralph L.
Goldstein, Arthur W.
Cullom, Richard R.
Lewis Research Center.

January 1959

"October 1959."Caption title.Includes bibliographical references (p. 16-17).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

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

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 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

Static sea-level performance of an axial-flow-compressor turbojet engine with an air-cooled turbine /

Cochran, Reeves P.
Dengler, Robert P.
Cochran, Reeves P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

"Declassified February 10, 1959.""March 15, 1955."Cover title.Includes bibliographical references (p...

Kohl, Robert C.
Larkin, Robert G., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "November 2, 1948."Includes bibliographical references: p. 4.Mode of access: Interne...

Experimental investigation of direct control of diffuser pressure on 16-inch ram-jet engine /

Dunbar, William R.
Hurrell, Herbert G.
Vasu, George.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 20, 1955."Includes bibliographical references (p. 24).Mode of access: Internet

Performance of compressor blade cascades at high Mach numbers /

Bogdonoff, Seymour M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1947

"June 12, 1947."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Performance comparisons of high mach number compressor rotor blading /

Gostelow, J. P.
Smith, L. H.
Krabacher, K. W.
Lewis Research Center.
General Electric Company.
United States. National Aeronautics and Space Administration.

January 1968

"December 1968."Includes bibliographical references."Prepared under contract no.Mode of access: Inte...

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...

Compressor-blade vibration and performance in a J47-23 turbojet engine under conditions of rotating stall /

Hanson, Morgan P.
Meyer, Andre J.
Johnson, Donald F.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1955

"June 13 1955."Includes bibliographical references (p. 7-8).Mode of access: Internet

Effect of high rotor pressure-surface diffusion on performance of a transonic turbine /

Abstract

Extracted data

Effect of high rotor pressure-surface diffusion on performance of a transonic turbine /

Abstract

Extracted data

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