Noise reduction tests of large scale model externally blown flap using trailing-edge blowing and partial flap slot covering /

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine /

Minner, Gene L. (Gene Logan), 1942-
Heidelberg, Laurence J.
Goldman, Richard G.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

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

Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing /

Stickle, Joseph W.
Henry, Robert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices /

McKinzie, Daniel J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover.STAR category 71."Lewis Research Center."Includes bibiliographical references.Mode...

Radiated noise from an externally blown flap /

Reddy, Narayana N., 1938-
Yu, James C.
Langley Research Center.

January 1975

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

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

A method for calculating externally blown flap noise /

Fink, Martin R.
United Technologies Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

March 1978.Contract NAS 3-17863.Includes bibliographical references (p. 50-51).Mode of access: Inter...

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft /

Falarski, Michael D.
Aoyagi, Kiyoshi.
Aiken, Thomas N.
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1975

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Gentry, Garl L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Includes bibliographical references (...

A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap /

Johnson, William G. (William Garland), 1944-
Kardas, Gerald E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration /

Paulson, John W.
Banks, Daniel W.
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."March 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine /

Minner, Gene L. (Gene Logan), 1942-
Heidelberg, Laurence J.
Goldman, Richard G.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

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

Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing /

Stickle, Joseph W.
Henry, Robert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Aeroacoustic performance of an externally blown flap configuration with several flap noise suppression devices /

McKinzie, Daniel J.
Lewis Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1982

"May 1982"--Cover.STAR category 71."Lewis Research Center."Includes bibiliographical references.Mode...

Radiated noise from an externally blown flap /

Reddy, Narayana N., 1938-
Yu, James C.
Langley Research Center.

January 1975

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

Wind-tunnel investigation of aerodynamic loads on a large-scale externally blown flap model and comparison with theory /

Perry, Boyd.
Greene, George C.
Langley Research Center.

January 1975

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode ...

A method for calculating externally blown flap noise /

Fink, Martin R.
United Technologies Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Office.

January 1978

March 1978.Contract NAS 3-17863.Includes bibliographical references (p. 50-51).Mode of access: Inter...

Noise characteristics of jet flap type exhaust flows /

Schrecker, G. O.
Maus, J. R.
Langley Research Center.
University of Tennessee (System). Space Institute.

January 1974

"Prepared by the University of Tennessee Space Institute ... for Langley Research Center."Cover titl...

Acoustic characteristics of a large-scale wind-tunnel model of a jet flap aircraft /

Falarski, Michael D.
Aoyagi, Kiyoshi.
Aiken, Thomas N.
U.S. Army Air Mobility Research and Development Laboratory.
Ames Research Center.

January 1975

Prepared at Ames Research Center and the U.S. Army Air Mobility R&D Laboratory.Cover title.Includes ...

Wind-tunnel investigation of an externally blown flap STOL transport model including an investigation of wall effects /

Gentry, Garl L.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Includes bibliographical references (...

A wind-tunnel investigation of the wake near the trailing edge of a deflected externally blown flap /

Johnson, William G. (William Garland), 1944-
Kardas, Gerald E.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Chiefly graphs.Cover title.Bibliography: p. 10.Mode of access: I...

Effect of wing aspect ratio and flap span on aerodynamic characteristics of an externally blown jet-flap STOL model /

Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 9.Mode of access: Internet

Investigation of trailing-edge-flap spanwise-blowing concepts on an advanced fighter configuration /

Paulson, John W.
Banks, Daniel W.
Quinto, P. Frank.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.

January 1984

Subject category 02."March 1984"--Cover.Distributed to depository libraries in microfiche.Includes b...

Wind-tunnel investigation of effects of variations in Reynolds number and leading-edge treatment on the aerodynamic characteristics of an externally blown jet-flap configuration /

Parlett, Lysle P.
Megrail, James L.
Smith, Charles Christian, 1921-
Langley Research Center.

January 1973

Research prepared at Langley Research Center.Cover title.Bibliography: p. 8.Mode of access: Internet

Effect of treated length on performance of full-scale turbofan inlet noise suppressors /

Dittmar, James H.
Groeneweg, John F. (John Frederick), 1937-
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 14-15).Mode of...

Noise suppression by an acoustically treated three-ring inlet on a TF-34 engine /

Minner, Gene L. (Gene Logan), 1942-
Heidelberg, Laurence J.
Goldman, Richard G.
Lewis Research Center.

January 1976

Cover title.Includes bibliographical references (p. 19-20).Mode of access: Internet

Longitudinal aerodynamic characteristics of an externally blown flap powered-lift model with several propulsive system simulators /

Hoad, Danny R.
Langley Research Center.

January 1974

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

Wind-tunnel study to explore the use of slot spoilers to modulate the flap-induced lift of a wing /

Stickle, Joseph W.
Henry, Robert C.
Langley Research Center.
United States. National Aeronautics and Space Administration.

January 1968

Cover title."July 1968."Includes bibliographical references (p. 5).Mode of access: Internet

Noise reduction tests of large scale model externally blown flap using trailing-edge blowing and partial flap slot covering /

Abstract

Extracted data

Noise reduction tests of large scale model externally blown flap using trailing-edge blowing and partial flap slot covering /

Abstract

Extracted data

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