Recent Advances in Aeroacoustics

Proceedings of an International Symposium held at Stanford University, August 22–26, 1983

A. Krothapalli, C.A. Smith (Herausgeber)

Buch | Softcover

511 Seiten

2011 | Softcover reprint of the original 1st ed. 1986
Springer-Verlag New York Inc.
978-1-4612-9324-8 (ISBN)

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The Joint Institute for Aeronautics and Acoustics at Stanford University was established in October 1973 to provide an academic environment for long-term cooperative research between Stanford and NASA Ames Research Center. Since its establishment, the Institute has conducted theoretical and experimental work in the areas of aerodynamics, acoustics, fluid mechanics, flight dynamics, guidance and control, and human factors. This research has involved Stanford faculty, research associates, graduate students, and many distinguished visitors in collaborative efforts with the research staff of NASA Ames Research Center. The occasion of the Institute's tenth anniversary was used to reflect back on where that research has brought us, and to consider where our endeavors should be directed next. Thus, an International Symposium was held to review recent advances in the fields relevant to the activities of the Institute and to discuss the areas of research to be undertaken in the future. This anniversary was also chosen as an opportunity to honor one of the Institute's founders and its director, Professor Krishnamurty Karamcheti. It has been his crea tive inspiration that has provided the ideal research environment at the Joint Institute.

I. Noise Due to Jets, Shear Layers, and Turbulence.- Waves in Turbulent Mixing Layers.- On Broadband Shock Associated Noise of Supersonic Jets.- On the Absorbtion of Sound by Turbulence and Other Hydrodynamic Flows.- II. Rotor Acoustics.- Analyses of Broadband Noise Mechanisms of Rotors.- The Evolution of Methods for Noise Prediction of High Speed Rotors and Propellers in the Time Domain.- Helicopter Impulsive Noise: Theoretical and Experimental Status.- III. Generation and Propagation.- The Development of Contemporary Views of Flow-Tone Generation.- A Simple Theory of the Sondhauss Tube.- A Review of Numerical Methods in Acoustic Wave Propagation.- Nonlinear Acoustic Propagation of Broadband Noise.- Acoustic Propagation in Partially Choked Ducts.

Co-Autor	W.K. Blake, S.M. Candel, D.G. Crigthon
Zusatzinfo	XII, 511 p.
Verlagsort	New York, NY
Sprache	englisch
Maße	155 x 235 mm
Themenwelt	Naturwissenschaften ► Physik / Astronomie ► Mechanik
	Technik ► Fahrzeugbau / Schiffbau
	Technik ► Luft- / Raumfahrttechnik
	Technik ► Maschinenbau
ISBN-10	1-4612-9324-3 / 1461293243
ISBN-13	978-1-4612-9324-8 / 9781461293248
Zustand	Neuware