Bücher zum Thema „Aeroacoustic noise“

Meyer, Harold D. Aeroacoustic analysis of turbofan noise generation. Cleveland, Ohio: Lewis Reserch Center, 1996.

G, Migliore Paul, und National Renewable Energy Laboratory (U.S.), Hrsg. Semi-empirical aeroacoustic noise prediction code for wind turbines. Golden, Colo: National Renewable Energy Laboratory, 2003.

S, Hultgren Lennart, und NASA Glenn Research Center, Hrsg. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

S, Hultgren Lennart, und NASA Glenn Research Center, Hrsg. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Loh, Ching Y. Computing jet screech--a complex aeroacoustic feedback system. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

W, Elliott Joe, Orie Nettie M, United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., United States. Army Aviation Systems Command. und Langley Research Center, Hrsg. 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.

United States. National Aeronautics and Space Administration., Hrsg. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., Hrsg. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., Hrsg. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., Hrsg. A large hemi-anechoic enclosure for community-compatible aeroacoustic testing of aircraft propulsion systems. [Washington, DC]: National Aeronautics and Space Administration, 1993.

Raman, Ganesh. Aeroacoustic characteristics of a rectangular multi-element supersonic jet mixer-ejector nozzle. [Washington, D.C.]: National Aeronautics and Space Administration, 1996.

S, Lyrintzis Anastasios, und United States. National Aeronautics and Space Administration., Hrsg. 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.

Migliore, Paul G. Wind tunnel aeroacoustic tests of six airfoils for use on small wind turbines: Preprint. Golden, Colo: National Renewable Energy Laboratory, 2003.

Douglas, Boyd D., und Langley Research Center, Hrsg. 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.

United States. National Aeronautics and Space Administration., Hrsg. Aeroacoustic diffraction and dissipation by a short propeller cowl in subsonic flight. [Washington, D.C.]: National Aeronautics and Space Administration, 1993.

S, Ukeiley Lawrence, Lee Sang W und Langley Research Center, Hrsg. Aeroacoustic data for a high Reynolds number axisymmetric subsonic jet. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

Ahuja, 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.

E, Hughes Christopher, und United States. National Aeronautics and Space Administration., Hrsg. 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.

Ganesh, Raman, Hrsg. Jet aeroacoustics. Essex, UK: Multi-Science Publication, 2008.

C, Hardin Jay, und Hussaini M. Yousuff, Hrsg. Computational aeroacoustics. New York: Springer-Verlag, 1993.

Center, Ames Research, Hrsg. Tilt rotor hover aeroacoustics. [Moffett Field, Calif.]: National Aeronautics and Space Administration, Ames Research Center, 1992.

United States. National Aeronautics and Space Administration., Hrsg. Aeroacoustics of advanced propellers. [Washington, D.C.]: NASA, 1990.

Goldstein, Marvin E. Aeroacoustics of subsonic turbulent shear flows. [Washington, DC]: National Aeronautics and Space Administration, 1987.

H, Hubbard Harvey, Hrsg. Aeroacoustics of flight vehicles: Theory and practice. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

H, Hubbard Harvey, und Acoustical Society of America, Hrsg. Aeroacoustics of flight vehicles: Theory and practice. Woodbury, NY: Published for the Acoustical Society of America through the American Institute of Physics, 1995.

United States. National Aeronautics and Space Administration., Hrsg. The aeroacoustics of supersonic coaxial jets. [Washington, DC]: National Aeronautics and Space Administration, 1994.

J, Anthoine, Hirschberg A und Von Karman Institute for Fluid Dynamics., Hrsg. Advances in aeroacoustics and applications: March 15-19, 2004. Rhode Saint Genese: Von Karman Institute for Fluid Dynamics, 2004.

National 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.

Dahl, Milo D. Assessment of NASA's aircraft noise prediction capability. Herausgegeben von NASA Glenn Research Center. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2012.

J, Lighthill M. Some aspects of the aeroacoustics of high-speed jets. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1993.

Geneviève, Comte-Bellot, Olivari D und Von Karman Institute for Fluid Dynamics., Hrsg. Aeroacoustics and active noise control: September 15-18, 1997. Rhode St. Genèse, Belgium: Von Karman Institute for Fluid Dynamics, 1997.

Russ, Repp, Weir Donald S und United States. National Aeronautics and Space Administration., Hrsg. Quiet high-speed fan. [Washington, DC: National Aeronautics and Space Administration, 1997.

Russ, Repp, Weir Donald S und United States. National Aeronautics and Space Administration., Hrsg. Quiet high-speed fan. [Washington, DC: National Aeronautics and Space Administration, 1997.

Computational aeroacoustics: A wave number approach. New York: Cambridge University Press, 2012.

Hoad, Danny R. Rotor performance characteristics from an aeroacoustics helicopter wind-tunnel test program. Hampton, Va: Langley Research Center, 1986.

Center, Lewis Research, Hrsg. Unified aeroacoustics analysis for high speed turboprop aerodynamics and noise. [Cleveland, Ohio?]: Lewis Research Center, 1991.

E, Turkel, und Lewis Research Center, Hrsg. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.

E, Turkel, und Lewis Research Center, Hrsg. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.

E, Turkel, und Lewis Research Center, Hrsg. High-accuracy compact MacCormack-type schemes for computational aeroacoustics. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Center, Langley Research, Hrsg. Fan noise prediction assessment. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

F, Ng Wing, und NASA Glenn Research Center, Hrsg. Fan noise control using Herschel-Quincke resonators. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Center, NASA Glenn Research, Hrsg. Turbofan noise propagation and radiation at high frequencies. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Division. und United States. Army Aviation Systems Command., Hrsg. 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.

H, Zysman Steven, Barber Thomas J und NASA Glenn Research Center, Hrsg. 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.

United States. National Aeronautics and Space Administration., Hrsg. 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.

Center, Langley Research, Hrsg. Noise exposure reduction of advanced high-lift systems. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1995.

Center, NASA Glenn Research, Hrsg. Computational aeroacoustics by the space-time CE/SE method. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Joint 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.

M, Gilinsky M., und United States. National Aeronautics and Space Administration., Hrsg. Nozzle thrust optimization while reducing jet noise. [Washington, D.C: National Aeronautics and Space Administration, 1995.

M, Gilinsky M., und United States. National Aeronautics and Space Administration., Hrsg. Nozzle thrust optimization while reducing jet noise. [Washington, D.C: National Aeronautics and Space Administration, 1995.