A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed /

Cooling of gas turbines

Wolfenstein, Lincoln
McCarthy, John S., joint author.
Maxwell, Robert L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 28, 1947."Includes bibliographical references: p. 22.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Monroe, William R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 18, 1947."Includes bibliographical references: p. 29.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Low-speed cascade investigation of loaded leading-edge compressor blades /

Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 11, 1956."Includes bibliographical references (p. 11).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

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

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...

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

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

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

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

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).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

Vibration survey of blades in 10-stage axial-flow compressor

Meyer, Andre J. Jr.
Calvert, Howard F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 31, 1949."Includes bibliographical references: p. 6.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...

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

Cooling of gas turbines

Wolfenstein, Lincoln
McCarthy, John S., joint author.
Meyer, Gene L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "March 18, 1947."Includes bibliographical references: p. 20.Mode of access: Internet

Cooling of gas turbines

Wolfenstein, Lincoln
McCarthy, John S., joint author.
Maxwell, Robert L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 28, 1947."Includes bibliographical references: p. 22.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Monroe, William R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 18, 1947."Includes bibliographical references: p. 29.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

Low-speed cascade investigation of loaded leading-edge compressor blades /

Emery, James C.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1956

"January 11, 1956."Includes bibliographical references (p. 11).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

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

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...

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

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

Investigation of an impulse axial-flow compressor rotor over a range of blade angles /

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

January 1950

"August 29, 1950."Cover title.Includes bibliographical references (p. 16).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

Vibration survey of blades in 10-stage axial-flow compressor

Meyer, Andre J. Jr.
Calvert, Howard F., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "January 31, 1949."Includes bibliographical references: p. 6.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...

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

Cooling of gas turbines

Wolfenstein, Lincoln
McCarthy, John S., joint author.
Meyer, Gene L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "March 18, 1947."Includes bibliographical references: p. 20.Mode of access: Internet

Cooling of gas turbines

Wolfenstein, Lincoln
McCarthy, John S., joint author.
Maxwell, Robert L., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 28, 1947."Includes bibliographical references: p. 22.Mode of access: Internet

Cooling of gas turbines

Brown, W. Byron
Monroe, William R., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Aircraft Engine Research Laboratory.

On front cover: "April 18, 1947."Includes bibliographical references: p. 29.Mode of access: Internet

Investigation of a gas turbine with National Bureau of Standards body 4811 ceramic rotor blades /

Freche, John C.
Sheflin, Bob W., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
United States. National Advisory Committee for Aeronautics.
Lewis Flight Propulsion Laboratory.

"October 28, 1948."Cover title.Includes bibliographical references (p. 12).Mode of access: Internet

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed /

Abstract

Extracted data

A comparison of typical National Gas Turbine Establishment and NACA axial-flow compressor blade sections in cascade at low speed /

Abstract

Extracted data

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