An analysis of control requirements and control parameters for direct-coupled turbojet engines /

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

An analysis of VG and VGH operational data from a twin-engine turboprop transport airplane /

Hunter, Paul A.
Walker, Walter G.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "February 17, 1948."Includes bibliographical references: p. 12-13.Mode of access: In...

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

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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 ...

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

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Golladay, Richard L.
Gendler, Stanley L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 25, 1948."Includes bibliographical references: p. 26-27.Mode of access: Inte...

Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8 /

Cavicchi, Richard H.
English, Robert E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Cover title.Includes bibliographical references (p. 33).Mode of...

An analysis of ducted-airfoil ram jets for supersonic aircraft /

Hill, Paul R.
Gammal, A. A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 7, 1948."Includes bibliographical references (p. 29).Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Esgar, Jack B.
Clure, John L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 8, 1952."Title from cover.Includes bibliographical references: p. 24-25.Mode of...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

An analysis of VG and VGH operational data from a twin-engine turboprop transport airplane /

Hunter, Paul A.
Walker, Walter G.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "February 17, 1948."Includes bibliographical references: p. 12-13.Mode of access: In...

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

Analysis of factors affecting selection and design of air-cooled single-stage turbines for turbojet engines

Hubbartt, James E.
Schramm, Wilson B., joint author.
Rossbach, Richard J., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "September 16, 1954."Title from cover.Includes bibliographical references: p. 24.Mod...

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 ...

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

Calculations of the performance of a compression-ignition engine-compressor turbine combination.

Mendelson, Alexander.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

Prepared at the Aircraft Engine Research Laboratory, Cleveland, Ohio.On front cover: "February 3, 19...

Investigation of the I-40 Jet-Propulsion Engine in the Cleveland Altitude Wind Tunnel

Golladay, Richard L.
Gendler, Stanley L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "August 25, 1948."Includes bibliographical references: p. 26-27.Mode of access: Inte...

Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8 /

Cavicchi, Richard H.
English, Robert E., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

On front cover: "September 24, 1954."Cover title.Includes bibliographical references (p. 33).Mode of...

An analysis of ducted-airfoil ram jets for supersonic aircraft /

Hill, Paul R.
Gammal, A. A.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1948

"July 7, 1948."Includes bibliographical references (p. 29).Mode of access: Internet

Experimental investigation of air-cooled turbine blades in turbojet engine

Esgar, Jack B.
Clure, John L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "May 8, 1952."Title from cover.Includes bibliographical references: p. 24-25.Mode of...

An analysis of the effects of aeroelasticity on static longitudinal stability and control of a swept-back-wing airplane /

Skoog, Richard B.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Ames Research Center.

On front cover: "August 27, 1951."Includes bibliographical references: p. 29.Mode of access: Interne...

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

Stability analysis and minimum thrust vector control requirements of booster vehicles during atmospheric flight /

Borsody, Janos.
Teren, Fred.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."May 1968."Includes bibliographical references (p. 42).Mode of access: Internet

Static investigation of several jet deflectors for longitudinal control of an aircraft /

Valerino, Alfred S.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "June 7, 1955."Title from cover.Includes bibliographical references: p. 9.Mode of ac...

An analysis of VG and VGH operational data from a twin-engine turboprop transport airplane /

Hunter, Paul A.
Walker, Walter G.
United States. National Aeronautics and Space Administration.

Cover title."July 1963."Includes bibliographical references.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Livingood, John N. B., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "February 17, 1948."Includes bibliographical references: p. 12-13.Mode of access: In...

An analysis of control requirements and control parameters for direct-coupled turbojet engines /

Abstract

Extracted data

An analysis of control requirements and control parameters for direct-coupled turbojet engines /

Abstract

Extracted data

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