Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

Conners, Timothy E.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Includes bibliographical references (p. 8).Mod...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Investigation of installation effects on single-engine convergent-divergent nozzles /

Burley, James R.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"November 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle /

Biesiadny, Thomas J.
Abdelwahab, Mahmood, joint author.
Grey, Rudolph E., joint author.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic performance of flared fan nozzles used as inlets /

Dietrich, Donald A.
Kelm, Gary G., joint author.
Keith, Theo G., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle /

Burley, Richard R.
Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression /

Huff, Ronald G.
Groesbeck, Donald E.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23).Mode of ac...

Flight velocity effects on jet noise of several variations of a twelve-chute suppressor installed on a plug nozzle /

Burley, Richard R.
Johns, Albert L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Noise and wake structure measurements in a subsonic tip speed fan /

Magliozzi, B.
Langley Research Center.
United Aircraft Corporation. Hamilton Standard Division.

January 1973

"Prepared by Hamilton Standard, Division of United Aircraft Corporation ... for Langley Research Cen...

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines.

Goldstein, Arthur W.
Balombin, Joseph R.
Lucas, James G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Low noise turbofan engine without aerodynamic blade loading.Includes bibliographical references (p. ...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers /

Pendergraft, Odis C.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"August 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

Conners, Timothy E.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Includes bibliographical references (p. 8).Mod...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Investigation of installation effects on single-engine convergent-divergent nozzles /

Burley, James R.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"November 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Altitude performance of a low-noise-technology fan in a turbofan engine with and without a sound suppressing nacelle /

Biesiadny, Thomas J.
Abdelwahab, Mahmood, joint author.
Grey, Rudolph E., joint author.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 17).Mode of access: Internet

Aerodynamic performance of flared fan nozzles used as inlets /

Dietrich, Donald A.
Kelm, Gary G., joint author.
Keith, Theo G., joint author.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 16).Mode of access: Internet

Flight velocity effects on jet noise of several variations of a 48-tube suppressor installed on a plug nozzle /

Burley, Richard R.
Head, Verlon L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Flight velocity effects on the jet noise of several variations of a 104-tube suppressor nozzle /

Burley, Richard R.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23-24).Mode of...

Cold-flow acoustic evaluation of a small-scale, divergent, lobed nozzle for supersonic jet noise suppression /

Huff, Ronald G.
Groesbeck, Donald E.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 23).Mode of ac...

Flight velocity effects on jet noise of several variations of a twelve-chute suppressor installed on a plug nozzle /

Burley, Richard R.
Johns, Albert L.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 17-18).Mode of...

Noise and wake structure measurements in a subsonic tip speed fan /

Magliozzi, B.
Langley Research Center.
United Aircraft Corporation. Hamilton Standard Division.

January 1973

"Prepared by Hamilton Standard, Division of United Aircraft Corporation ... for Langley Research Cen...

Measurement of performance, inlet flow characteristics, and radiated noise for a turbojet engine having choked inlet flow /

Cawthorn, Jimmy M.
Hayes, Clyde.
Morris, Garland J.
United States. National Aeronautics and Space Administration.
Langley Research Center.

January 1967

Performed at Langley Research Center."May 1967."Includes bibliographical references (p. 16).Mode of ...

Low-speed wind-tunnel investigation of a four-engine upper surface blown model having a swept wing and rectangular and D-shaped exhaust nozzles /

Sleeman, William C.
Hohlweg, William C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 18).Mode of ...

Acoustic and aerodynamic performance of a 6-foot-diameter fan for turbofan engines.

Goldstein, Arthur W.
Balombin, Joseph R.
Lucas, James G.
Lewis Research Center.
United States. National Aeronautics and Space Administration.

January 1970

Low noise turbofan engine without aerodynamic blade loading.Includes bibliographical references (p. ...

Exhaust-nozzle characteristics for a twin-jet variable-wing-sweep fighter airplane model at Mach numbers to 2.2 /

Reubush, David E.
Mercer, Charles E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 15).Mode of ...

Effect of nozzle and vertical-tail variables on the performance of a three-surface F-15 model at transonic Mach numbers /

Pendergraft, Odis C.
Bare, E. Ann.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"August 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine /

Conners, Timothy E.
Dryden Flight Research Facility.

January 1989

Research performed at Dryden Flight Research Facility.Includes bibliographical references (p. 8).Mod...

Fluctuating pressures on fan blades of a turbofan engine : flight test investigation /

Schoenster, James A.
Langley Research Center.

January 1985

Prepared at Langley Research Center."February 1985"--Cover.Includes bibliographical references (p. 7...

Investigation of installation effects on single-engine convergent-divergent nozzles /

Burley, James R.
Berrier, Bobby L.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"November 1982"--Cover.Includes bibliographical references.Mode of access: Internet

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /

Abstract

Extracted data

Acoustic, performance, and wake survey measurements of a lobed velocity-decayer nozzle installed on a quieted TF-34 turbofan engine /

Abstract

Extracted data

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