An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation /

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).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

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 an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F /

Cochran, Reeves P.
Dengler, Robert P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Propulsion system elements; Propulsion systems, air-jet.Includes bibliograph...

Experimental investigation of air-cooled turbine blades in turbojet engine

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

On front cover: "April 2, 1951."Title from cover.Includes bibliographical references: p. 21.Mode of ...

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 experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

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...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

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....

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).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

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).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

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 an air-cooled turbine operating in a turbojet engine at turbine inlet temperatures up to 2500 degrees F /

Cochran, Reeves P.
Dengler, Robert P.
United States. National Aeronautics and Space Administration.

Cover title."July 1961."Propulsion system elements; Propulsion systems, air-jet.Includes bibliograph...

Experimental investigation of air-cooled turbine blades in turbojet engine

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

On front cover: "April 2, 1951."Title from cover.Includes bibliographical references: p. 21.Mode of ...

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 experimental investigation of the flow in an axisymmetric internal-compression inlet for M=2.75 /

Watson, Earl C.
Peterson, William P.
United States. National Aeronautics and Space Administration.

Cover title."April 1961."Fluid mechanics; Propulsion system elements.Includes bibliographical refere...

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...

Aerodynamic loads on an isolated shrouded-propeller configuration of angles of attack from -10 degrees to 110 degrees /

Grunwald, Kalman J.
Goodson, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."January 1962."Aerodynamics, aircraft; Aircraft; Propulsion systems, air-jet.Includes bi...

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....

A wind-tunnel investigation of a 4-foot-diameter ducted fan mounted on the tip of a semispan wing /

Yaggy, Paul F.
Mort, Kenneth W.
United States. National Aeronautics and Space Administration.

Cover title."March 1961."Aircraft; Propulsion systems, air-jet; Stability and control;Includes bibli...

Preliminary results of aerodynamic heating studies on the X-15 airplane /

Banner, Richard D.
Quinn, Robert D.
Kuhl, Albert E.
Flight Research Center (U.S.)

January 1962

"March 1962."Cover title.Includes bibliographical references (p. 12).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

An experimental study of the effect of downwash from a twin-propeller VTOL aircraft on several types of ground surfaces /

O'Bryan, Thomas C.
United States. National Aeronautics and Space Administration.

Cover title."May 1962."Aerodynamics, aircraft; Aircraft; Piloting.Includes bibliographical reference...

Test-engine and inlet performance of an aircraft used for investigating flight effects on fan noise /

Golub, Robert A.
Preisser, John S.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 71."April 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Transonic flutter investigation of models of the X-15 airplane horizontal tail /

Young, Lou S.
Bland, Samuel R.
Langley Research Center.

January 1961

"February 1961."Caption title.Includes bibliographical references (p. 14).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 experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation /

Abstract

Extracted data

An experimental investigation of the aerodynamics and cooling of a horizontally-opposed air-cooled aircraft engine installation /

Abstract

Extracted data

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