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

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

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

Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions /

Hanson, Morgan P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"December 23,1955."Includes bibliographical references (p. 11).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

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

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

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

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

Investigation of an impulse axial-flow compressor /

Erwin, John R.
Schulze, Wallace M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"February 8, 1950."Includes bibliographical references (p. 22).Mode of access: Internet

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

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...

Performance of J33 turbojet engine with shaft-power extraction

Ross, Albert O.
Nettles, J. Cary, joint author.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 24, 1948."Includes bibliographical references: p. 10.Mode of access: Interne...

Performance of J33 turbojet engine with shaft-power extraction

Nettles, J. C.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "May 28, 1948."Includes bibliographical references: p. 11.Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

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

Compressor-blade vibration of a J57-P-1 turbojet engine during exploratory operation with inlet-pressure distortions /

Hanson, Morgan P.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"December 23,1955."Includes bibliographical references (p. 11).Mode of access: Internet

Performance of a turbojet engine in combination with an external-internal-compression inlet to mach 2.88 /

Bowditch, David N.
Tabata, William K.
Anderson, Bernhard H.
United States. National Aeronautics and Space Administration.

"July 1960."Cover title.Includes bibliographical references (p. 10-11).Mode of access: Internet

Experimental investigation of flow through three highly loaded inlet guide vanes having different spanwise circulation gradients /

Beatty, Loren A.
Emery, James C.
Savage, Melvyn.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.

January 1952

"July 28, 1952."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

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

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

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

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

Investigation of an impulse axial-flow compressor /

Erwin, John R.
Schulze, Wallace M.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1950

"February 8, 1950."Includes bibliographical references (p. 22).Mode of access: Internet

Investigation of acceleration characteristics of a single-spool turbojet engine /

Oppenheimer, Frank L.
Pack, George J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "October 26, 1953."Title from cover.Includes bibliographical references: p. 13.Mode ...

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...

Performance of J33 turbojet engine with shaft-power extraction

Ross, Albert O.
Nettles, J. Cary, joint author.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 24, 1948."Includes bibliographical references: p. 10.Mode of access: Interne...

Performance of J33 turbojet engine with shaft-power extraction

Nettles, J. C.
Easterly, J. R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "May 28, 1948."Includes bibliographical references: p. 11.Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Stepka, Francis S.
Clure, John L., joint author.
Bear, H. Robert joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Title from cover.Includes bibliographical references: p. 14-15....

The performance of conical supersonic scoop inlets on circular fuselages /

Hasel, Lowell E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"November 17, 1953."Includes bibliographical references (p. 7).Mode of access: Internet

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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