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

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.Mode of access: Internet

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

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

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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

Novik, David
Otto, Edward W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "February 18, 1948."Includes bibliographical references: p. 23-24.Mode of access: In...

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...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).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

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings /

Radin, Edward J.
Carpenter, Paul J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"October 7, 1953."Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of ram-jet-engine time delay following a fuel-flow disturbance /

Wilcox, Fred A.
Anderson, Arthur R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 30, 1955."Includes bibliographical references (p. 15-16).Mode of access: Internet

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

Mayer, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

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...

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...

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.Mode of access: Internet

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

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

Free-jet tests of a 1.1-inch-diameter supersonic ram-jet engine /

Judd, Joseph H.
Trout, Otto F.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"March 5, 1952."Includes bibliographical references (p. 8).Mode of access: Internet

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

Novik, David
Otto, Edward W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Flight Propulsion Research Laboratory.

On front cover: "February 18, 1948."Includes bibliographical references: p. 23-24.Mode of access: In...

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...

Preliminary results of supersonic-jet tests of simplified wing structures /

Heldenfels, Richard R.
Rosecrans, Richard.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"July 8, 1953."Includes bibliographical references (p. 15).Mode of access: Internet

Flight investigation of the zero-lift drag of two ram-jet missile configurations at Mach numbers from 1.0 to 1.89 /

Brown, Clarence A.
Bressette, Walter E.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"March 9, 1953."Includes bibliographical references (p. 10).Mode of access: Internet

Preliminary investigation of effects of combustion in ram jet on performance of supersonic diffusers.

Schroeder, Albert H.
Connors, James F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 22, 1948."Title from cover.Includes bibliographical references (p. 6).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

Comparison of the performance of a helicopter-type ram-jet engine under various centrifugal loadings /

Radin, Edward J.
Carpenter, Paul J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1953

"October 7, 1953."Includes bibliographical references (p. 9).Mode of access: Internet

An analysis of ram-jet-engine time delay following a fuel-flow disturbance /

Wilcox, Fred A.
Anderson, Arthur R.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"June 30, 1955."Includes bibliographical references (p. 15-16).Mode of access: Internet

Estimation of lift and drag of airfoils at near sonic speeds and in the presence of detached shock waves /

Mayer, John P.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1949

"February 23, 1949."Includes bibliographical references (p. 12).Mode of access: Internet

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...

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...

Analysis of a bypass air control system for a supersonic mixed-compression inlet /

Brown, Stuart C.
United States. National Aeronautics and Space Administration.

Cover title."June 1967."Includes bibliographical references.Mode of access: Internet

The effects of a small jet of air exhausting from the nose of a body of revolution in supersonic flow /

Love, Eugene S.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1952

"November 12, 1952."Includes bibliographical references (p. 16).Mode of access: Internet

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

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

Abstract

Extracted data

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

Abstract

Extracted data

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