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

Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration /

Heyson, Harry H.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 32-34).Mode ...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Aerodynamic performance of 0.5-meter-diameter, 337-meter-per-second tip speed, 1.5-pressure-ratio, single-stage fan designed for low noise aircraft engines /

Gelder, Thomas F.
Lewis, George W., Jr.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode of...

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

Hanson, Donald B.
Langley Research Center.
United Technologies Corporation. Hamilton Standard Division.

"Prepared by Hamilton Standard ... for Langley Research Center.""August 1975."Cover title.Includes b...

Measurement and analysis of aircraft far-field aerodynamic noise /

Healy, Gerald J.
Langley Research Center.
Lockheed-California Company.

January 1974

"Prepared by Lockheed-California Company ... for Langley Research Center."Cover title.Bibliography: ...

Experimental and theoretical studies of subsonic fan noise /

Mani, R.
Bekofske, K., joint author.
General Electric Company.
Lewis Research Center.

January 1976

Prepared by General Electric Company, Schenectady, N.Y., for Lewis Research Center.Cover title.Inclu...

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...

Aircraft propeller induced structure-borne noise /

Unruh, James F.
Langley Research Center.
Southwest Research Institute.

January 1989

Prepared at Southwest Research Institute for Langley Research Center under Contract NAS1-17921.Bibli...

Theoretical studies of tone noise from a fan rotor /

Rao, G. V. R.
Digumarthi, R. V.
Chu, W. T., 1935-
Ames Research Center.
Rao and Associates.

January 1973

"Prepared by Rao and Associates ... for Ames Research Center."Cover title.Bibliography: p. 57-58.Mod...

Low-speed jet noise from a 1.83-meter (6-ft) fan for tubrofan engines /

Minner, Gene L. (Gene Logan), 1942-
Feiler, Charles E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

Simulated indoor sonic booms judged relative to noise from subsonic aircraft /

Kryter, Karl D.
Lukas, Jerome S., 1930-
Langley Research Center.
Stanford Research Institute.

January 1972

"Prepared by Stanford Research Institute ... for Langley Research Center."Cover title.Bibliography: ...

Investigation of the effects of inlet shapes on fan noise radiation /

Clark, T. L.
Vaidya, P. G.
Slotboom, D. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"Langley Research Center.""Prepared for Langley Research Center under contract NAS1-15394."Includes ...

Noise data from tests of a 1.83-meter- (6-ft-) diameter variable-pitch 1.2 pressure-ratio fan (QF-9) /

Glaser, Frederick W.
Friedman, Robert, 1929-
Wazyniak, Joseph A.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Chiefly statistical tables.Cover title.Bibliography: p. 7.Mode of ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration /

Heyson, Harry H.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 32-34).Mode ...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Aerodynamic performance of 0.5-meter-diameter, 337-meter-per-second tip speed, 1.5-pressure-ratio, single-stage fan designed for low noise aircraft engines /

Gelder, Thomas F.
Lewis, George W., Jr.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode of...

Study of noise sources in a subsonic fan using measured blade pressures and acoustic theory /

Hanson, Donald B.
Langley Research Center.
United Technologies Corporation. Hamilton Standard Division.

"Prepared by Hamilton Standard ... for Langley Research Center.""August 1975."Cover title.Includes b...

Measurement and analysis of aircraft far-field aerodynamic noise /

Healy, Gerald J.
Langley Research Center.
Lockheed-California Company.

January 1974

"Prepared by Lockheed-California Company ... for Langley Research Center."Cover title.Bibliography: ...

Experimental and theoretical studies of subsonic fan noise /

Mani, R.
Bekofske, K., joint author.
General Electric Company.
Lewis Research Center.

January 1976

Prepared by General Electric Company, Schenectady, N.Y., for Lewis Research Center.Cover title.Inclu...

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...

Aircraft propeller induced structure-borne noise /

Unruh, James F.
Langley Research Center.
Southwest Research Institute.

January 1989

Prepared at Southwest Research Institute for Langley Research Center under Contract NAS1-17921.Bibli...

Theoretical studies of tone noise from a fan rotor /

Rao, G. V. R.
Digumarthi, R. V.
Chu, W. T., 1935-
Ames Research Center.
Rao and Associates.

January 1973

"Prepared by Rao and Associates ... for Ames Research Center."Cover title.Bibliography: p. 57-58.Mod...

Low-speed jet noise from a 1.83-meter (6-ft) fan for tubrofan engines /

Minner, Gene L. (Gene Logan), 1942-
Feiler, Charles E.
United States. National Aeronautics and Space Administration.
Lewis Research Center.

January 1971

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 8-9).Mode of a...

Simulated indoor sonic booms judged relative to noise from subsonic aircraft /

Kryter, Karl D.
Lukas, Jerome S., 1930-
Langley Research Center.
Stanford Research Institute.

January 1972

"Prepared by Stanford Research Institute ... for Langley Research Center."Cover title.Bibliography: ...

Investigation of the effects of inlet shapes on fan noise radiation /

Clark, T. L.
Vaidya, P. G.
Slotboom, D. R.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch.
Langley Research Center.

January 1981

"Langley Research Center.""Prepared for Langley Research Center under contract NAS1-15394."Includes ...

Noise data from tests of a 1.83-meter- (6-ft-) diameter variable-pitch 1.2 pressure-ratio fan (QF-9) /

Glaser, Frederick W.
Friedman, Robert, 1929-
Wazyniak, Joseph A.
Lewis Research Center.

January 1975

Prepared at Lewis Research Center.Chiefly statistical tables.Cover title.Bibliography: p. 7.Mode of ...

Subsonic roll-damping characteristics of a series of wings /

Boyden, Richmond P.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 10-11).Mode ...

Flutter analysis of swept-wing subsonic aircraft with parameter studies of composite wings /

Housner, Jerrold M.
Stein, Manuel.
Langley Research Center.

January 1974

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 93).Mode of ...

Theoretical and experimental investigation of the performance of a fan-in-wing VTOL configuration /

Heyson, Harry H.
Langley Research Center.

January 1973

Prepared at Langley Research Center.Cover title.Includes bibliographical references (p. 32-34).Mode ...

Flight test measurements and analysis of sonic boom phenomena near the shock wave extremity /

Haglund, George T. (George Thomas)
Kane, Edward J.
Langley Research Center.
Boeing Company.

January 1973

"Prepared by the Boeing Company ... for Langley Research Center."Cover title.Bibliography: p. 85-88....

Aerodynamic performance of 0.5-meter-diameter, 337-meter-per-second tip speed, 1.5-pressure-ratio, single-stage fan designed for low noise aircraft engines /

Gelder, Thomas F.
Lewis, George W., Jr.
Lewis Research Center.

January 1974

Prepared at Lewis Research Center.Cover title.Includes bibliographical references (p. 33-34).Mode of...

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

Abstract

Extracted data

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

Abstract

Extracted data

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