Experimental investigation of a transonic compressor cascade and test results for four blade sections /

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

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

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

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

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...

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

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

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

Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness-chord ratio /

Goldberg, Theodore J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 4, 1955."Includes bibliographical references (p. 12).Mode of access: Internet

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Experimental investigation of a transonic axial-flow-compressor rotor with double-circular-arc airfoil blade sections.

Lewis, George W., Jr.
Serovy, G. K. (George K.)
Schwenk, Francis C.
Lewis Flight Propulsion Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1954

"Declassified October 31, 1958.""April 5, 1954."Cover title.Includes bibliographical references (p. ...

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

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

Experimental investigation of air-cooled turbine blades in turbojet engine

Hickel, Robert O.
Smith, Gordon T., joint author.
United States. National Advisory Committee for Aeronautics. NACA research memorandum.
Lewis Flight Propulsion Laboratory.

On front cover: "December 11, 1950."Title from cover.Includes bibliographical references: p. 15.Mode...

Experimental investigation of advanced concepts to increase turbine blade loading.

Lueders, H. G. (Howard George)

"April 1969"--cover.Includes bibliographical references.Mode of access: Internet

An experimental investigation of aerodynamic effects of airfoil thickness on transonic flutter characteristics /

Doggett, Robert V.
Morgan, Homer G.
Rainey, A. Gerald.
Langley Research Center.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 11-12).Mode of access: Internet

Experimental investigation of the transonic flutter of simple thin truncated-cone panels /

Gilman, Jean.
Langley Research Center.

January 1961

"October 1961."Cover title.Includes bibliographical references (p. 13).Mode of access: Internet

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...

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

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

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

Experimental investigation of an axial-flow supersonic compressor having sharp leading-edge blades with an 8-percent mean thickness-chord ratio /

Goldberg, Theodore J.
Langley Aeronautical Laboratory.
United States. National Adviosry Committee for Aeronautics. NACA research memorandum.

January 1955

"February 4, 1955."Includes bibliographical references (p. 12).Mode of access: Internet

An investigation of transonic flow fields surrounding hot and cold sonic jets /

Lee, George.
Ames Research Center.

Prepared at Ames Research Center."April 1961."Cover title.Includes bibliographical references (p. 18...

Performance of inlet stage of transonic compressor /

Urasek, Donald C.
Lewis, George W., Jr.
Steinke, Ronald J.
Lewis Research Center.

January 1976

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17).Mode of ac...

Experimental investigation of two-stage air-cooled turbine suitable for flight at Mach 2.5 /

Schum, Harold J.
Nunamaker, Robert R.
Petrash, Donald A.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1959

"November 1959."Cover title.Includes bibliographical references (p. 27).Mode of access: Internet

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Abstract

Extracted data

Experimental investigation of a transonic compressor cascade and test results for four blade sections /

Abstract

Extracted data

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