Книги з теми "Aeroacoustic noise"
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Meyer, Harold D. Aeroacoustic analysis of turbofan noise generation. Cleveland, Ohio: Lewis Reserch Center, 1996.
Знайти повний текст джерелаG, Migliore Paul, and National Renewable Energy Laboratory (U.S.), eds. Semi-empirical aeroacoustic noise prediction code for wind turbines. Golden, Colo: National Renewable Energy Laboratory, 2003.
Знайти повний текст джерелаS, Hultgren Lennart, and NASA Glenn Research Center, eds. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаS, Hultgren Lennart, and NASA Glenn Research Center, eds. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаLoh, Ching Y. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаW, Elliott Joe, Orie Nettie M, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., United States. Army Aviation Systems Command., and Langley Research Center, eds. Rotor performance characteristics from an aeroacoustic helicopter wind-tunnel test program. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаRaman, Ganesh. Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаS, Lyrintzis Anastasios, and United States. National Aeronautics and Space Administration., eds. Development of improved surface integral methods for jet aeroacoustic predictions: Final report, NASA-Langley grant no. NAG-1660. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаMigliore, Paul G. Wind tunnel aeroacoustic tests of six airfoils for use on small wind turbines: Preprint. Golden, Colo: National Renewable Energy Laboratory, 2003.
Знайти повний текст джерелаDouglas, Boyd D., and Langley Research Center, eds. Aeroacoustic codes for rotor harmonic and BVI noise - CAMRAD.Mod1/HIRES: Methodology and users' manual. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1998.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight. [Washington, D.C.]: National Aeronautics and Space Administration, 1993.
Знайти повний текст джерелаS, Ukeiley Lawrence, Lee Sang W, and Langley Research Center, eds. Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.
Знайти повний текст джерелаAhuja, K. K. Effects of cavity dimensions, boundary layer, and temperature on cavity noise with emphasis on benchmark data to validate computational aeroacoustic codes. Hampton, Va: Langley Research Center, 1995.
Знайти повний текст джерелаE, Hughes Christopher, and United States. National Aeronautics and Space Administration., eds. Aeroacoustic effects of reduced aft tip speed at constant thrust for a model counterrotation turboprop at takeoff conditions. [Washington, DC]: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаGanesh, Raman, ed. Jet aeroacoustics. Essex, UK: Multi-Science Publication, 2008.
Знайти повний текст джерелаC, Hardin Jay, and Hussaini M. Yousuff, eds. Computational aeroacoustics. New York: Springer-Verlag, 1993.
Знайти повний текст джерелаCenter, Ames Research, ed. Tilt rotor hover aeroacoustics. [Moffett Field, Calif.]: National Aeronautics and Space Administration, Ames Research Center, 1992.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Aeroacoustics of advanced propellers. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаGoldstein, Marvin E. Aeroacoustics of subsonic turbulent shear flows. [Washington, DC]: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаH, Hubbard Harvey, ed. Aeroacoustics of flight vehicles: Theory and practice. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Знайти повний текст джерелаH, Hubbard Harvey, and Acoustical Society of America, eds. Aeroacoustics of flight vehicles: Theory and practice. Woodbury, NY: Published for the Acoustical Society of America through the American Institute of Physics, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. The aeroacoustics of supersonic coaxial jets. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаJ, Anthoine, Hirschberg A, and Von Karman Institute for Fluid Dynamics., eds. Advances in aeroacoustics and applications: March 15-19, 2004. Rhode Saint Genese: Von Karman Institute for Fluid Dynamics, 2004.
Знайти повний текст джерелаNational Conference on Noise Control Engineering (12th 1993 Williamsburg, Va.). NOISE-CON 93 proceedings, 1993 National Conference on Noise Control Engineering: Noise control in aeroacoustics. New York, N.Y: Noise Control Foundation, c1993., 1993.
Знайти повний текст джерелаDahl, Milo D. Assessment of NASA's aircraft noise prediction capability. Edited by NASA Glenn Research Center. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2012.
Знайти повний текст джерелаJ, Lighthill M. Some aspects of the aeroacoustics of high-speed jets. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.
Знайти повний текст джерелаGeneviève, Comte-Bellot, Olivari D, and Von Karman Institute for Fluid Dynamics., eds. Aeroacoustics and active noise control: September 15-18, 1997. Rhode St. Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1997.
Знайти повний текст джерелаRuss, Repp, Weir Donald S, and United States. National Aeronautics and Space Administration., eds. Quiet high-speed fan. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаRuss, Repp, Weir Donald S, and United States. National Aeronautics and Space Administration., eds. Quiet high-speed fan. [Washington, DC: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаComputational aeroacoustics: A wave number approach. New York: Cambridge University Press, 2012.
Знайти повний текст джерелаHoad, Danny R. Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test program. Hampton, Va: Langley Research Center, 1986.
Знайти повний текст джерелаCenter, Lewis Research, ed. Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. [Cleveland, Ohio?]: Lewis Research Center, 1991.
Знайти повний текст джерелаE, Turkel, and Lewis Research Center, eds. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаE, Turkel, and Lewis Research Center, eds. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаE, Turkel, and Lewis Research Center, eds. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаCenter, Langley Research, ed. Fan noise prediction assessment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаF, Ng Wing, and NASA Glenn Research Center, eds. Fan noise control using Herschel-Quincke resonators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Turbofan noise propagation and radiation at high frequencies. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.
Знайти повний текст джерелаUnited 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.
Знайти повний текст джерелаH, Zysman Steven, Barber Thomas J, and NASA Glenn Research Center, eds. Large Engine Technology (LET) task XXXVII low-bypass ratio mixed turbofan engine subsonic jet noise reduction program test report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Jet aeroacoustics: Noise generation mechanism and prediction : progress report on NASA grant NAG1-1776, period covered by this report January 1, 1996 to December 31, 1996. [Washington, DC: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаCenter, Langley Research, ed. Noise exposure reduction of advanced high-lift systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Computational aeroacoustics by the space-time CE/SE method. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Знайти повний текст джерелаJoint CEAS/AIAA Aeroacoustics Conference (3rd 1997 Atlanta, Ga.). A collection of technical papers: 3rd AIAA/CEAS Aeroacoustics Conference : May 12-14, 1997/Atlanta, GA. Reston, Va: American Institute of Aeronautics and Astronautics, 1997.
Знайти повний текст джерелаM, Gilinsky M., and United States. National Aeronautics and Space Administration., eds. Nozzle thrust optimization while reducing jet noise. [Washington, D.C: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаM, Gilinsky M., and United States. National Aeronautics and Space Administration., eds. Nozzle thrust optimization while reducing jet noise. [Washington, D.C: National Aeronautics and Space Administration, 1995.
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