Libri sul tema "Aircraft cabins Noise Measurement"

Soderman, Paul T. J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Soderman, Paul T. J-85 jet engine noise measured in the ONERA S1 wind tunnel and extrapolated to far field. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.

Brase, L. O. Exhaust environment measurements of a turbofan engine equipped with an afterburner and 2D nozzle. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.

Block, P. J. W. Directory and trends of noise generated by a propeller in a wake. Hampton, Va: Langley Research Center, 1986.

Tubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.

Tubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.

Tubbs, Randy L. Horizon Air, Seattle, Washington. [Atlanta, Ga.]: Dept. of Health and Human Services, Centers for Disease Control and Prevention, National Institute for Occupational Safety and Health, 2004.

Kraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Kraft, R. E. Acoustic treatment design scaling methods. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

F, Martini K., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Structureborne noise measurements on a small twin-engine aircraft. [Washington, DC]: National Aeronautics and Space Administration, Scientific and Technical Information Division, 1988.

G, Rackl Robert, Andrianov Eduard V, and Langley Research Center, eds. Flight test measurements from the Tu-144LL structure/cabin noise experiment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2000.

Aliabadi, M. H., and Ignazio Dimino. Active Control of Aircraft Cabin Noise. Imperial College Press, 2015.

United States. National Aeronautics and Space Administration., ed. Asymptotic modal analysis of a rectangular acoustic cavity. [Washington, DC: National Aeronautics and Space Administration, 1988.

B, Bliss Donald, and United States. National Aeronautics and Space Administration., eds. Aircraft interior noise reduction by alternate resonance tuning: Progress report for the period ending December, 1990 : final progress report. Durham, NC: Dept. of Mechanical Engineering and Materials Science, Duke University, 1990.

Interaction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.

Center, Langley Research, ed. Interaction of airborne and structureborne noise radiated by plates. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. Interaction of airborne and structureborne noise radiated by plates. [Washington, DC]: National Aeronautics and Space Administration, 1986.

R, Fuller C., and United States. National Aeronautics and Space Administration., eds. An improved source model for aircraft interior noise studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

Laboratory test and acoustic analysis of cabin treatment for propfan test assessment aircraft. Burbank, Calif: Lockheed Aeronautical Systems Company, 1991.

1870-1952, Tillema H. F., MacGregor G. R, and Langley Research Center, eds. Application of analysis techniques for low frequency interior noise and vibration of commercial aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development., ed. Aircraft exterior noise measurement and analysis techniques. Neuilly sur Seine, France: AGARD, 1991.

Center, Langley Research, ed. Signal processing of aircraft flyover noise. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1991.

A, Clevenson Sherman, Stephens David G, and Langley Research Center, eds. The development of interior noise and vibration criteria. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1990.

1870-1952, Tillema H. F., Marshall Steven E, Langley Research Center, and Boeing Commercial Airplane Company, eds. Evaluation of analysis techniques for low frequency interior noise and vibration of commercial aircraft. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1989.

United States. National Aeronautics and Space Administration., ed. Combustion noise from gas turbine aircraft engines measurement of far-field levels. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.

U.S. Department of Transportation. Aircraft Source Noise Measurement Studies: Summary of Measurements, Data and Analysis. CreateSpace Independent Publishing Platform, 2013.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. and United States. Army Aviation Systems Command., eds. Measurement resolution of noise directivity patterns from acoustic flight tests. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.

T, Ohler Eric, and Construction Engineering Research Laboratories (U.S.), eds. Software development plan for the Assessment System for Aircraft Noise, version 2.0. [Champaign, Ill.]: US Army Corps of Engineers, Construction Engineering Research Laboratories, 1996.

M, Golebiowski, Seiner John M, and United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

M, Golebiowski, Seiner John M, and United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

M, Golebiowski, Seiner John M, and United States. National Aeronautics and Space Administration., eds. On the two components of turbulent mixing noise from supersonic jets. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.

Center, Langley Research, ed. Comparison of advanced turboprop and conventional jet and propeller aircraft flyover noise annoyance: Preliminary results. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

1961-, Schein David B., Gridley Doreen, Langley Research Center, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Analytical study of acoustic response of a semireverberant enclosure with application to active noise control. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

A, Haering Edward, and Hugh A. Dryden Flight Research Center., eds. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

A, Haering Edward, and Hugh A. Dryden Flight Research Center., eds. Ground-recorded sonic boom signatures of F-18 aircraft in formation flight. Edwards, Calif: National Aeronautics and Space Administration, Dryden Flight Research Center, 1995.

The accuracy of parameter estimation in system identification of noisy aircraft load measurement. [Los Angeles, Calif.]: University of California, Los Angeles, 1994.

H, Saiyed Naseem, and United States. National Aeronautics and Space Administration., eds. Characteristics of residual mixing noise from internal fan/core mixers. [Washington, DC]: National Aeronautics and Space Administration, 1997.

F, Peretti Linda, and United States. National Aeronautics and Space Administration., eds. Asymptotic modal analysis and statistical energy analysis. [Washington, DC: National Aeronautics and Space Administration, 1990.

E, Kraft R., and Langley Research Center, eds. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

E, Kraft R., and Langley Research Center, eds. Acoustic treatment design scaling methods: Phase II final report. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 2003.

Center, Langley Research, ed. Analysis of Particle Image Velocimetry (PIV) data for application to subsonic jet noise studies. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1997.

United States. National Aeronautics and Space Administration., ed. Experimental measurement of structural power flow on an aircraft fuselage: Progress report, grant number NAG-1-685. Boca Rotan, Fla: Florida Atlantic University, College of Engineering, Dept. of Ocean Engineering, Center for Acoustics and Vibrations, 1989.