Aerodynamic Noise / / ed. by H.S. Ribner.

• Superior document: Title is part of eBook package: De Gruyter University of Toronto Press eBook-Package Archive 1933-1999
• MitwirkendeR: Andersson, A.O.,; Caughey, David A.,; Coles, G. M.,; Cuadra, Elizabeth,; Dosanjh, Darshan S.,; Gedge, M. R.,; Grande, E.,; Gray, Larry,; Hawkins, S.J.,; Hayes, Wallace D.,; Hicks, J.A.,; Hubbard, Harvey H.,; Jones, Ian S. F.,; Kobrynski, M.,; Krishnappa, G.,; Large, J.B.,; Leehey, Patrick,; Lowson, M. V.,; Maestrello, L.,; Magliozzi, Bernard,; Metzger, Frederick B.,; Ollerhead, J. B.,; Reddaway, A.R.F.,; Resler, E. L.,; Ribner, H.S.,; Rice, Edward J.,; Slutsky, S.,; Towle, George B.,; Westley, R.,; Wilby, J. F.,; Williams, J. E. Ffowcs,; Woolley, J. H.,; Yu, James C.,
• HerausgeberIn: Ribner, H.S.,
• Place / Publishing House: Toronto : : University of Toronto Press, , [2019]; ©1969
• Year of Publication: 2019
• Language: English
• Series: Heritage
• Physical Description: 1 online resource (456 p.)
• Other title: Frontmatter --; FOREWORD --; PREFACE --; CONTENTS --; JETS AND NOISE --; THE DEVELOPMENT OF ENGINEERING PRACTICES IN JET, COMPRESSOR, AND BOUNDARY LAYER NOISE --; SCALES PERTINENT TO NOISE GENERATION FROM A JET --; ESTIMATION OF THE INTENSITY OF NOISE RADIATED FROM A SUBSONIC CIRCULAR JET --; GENERAL METHOD FOR CALCULATING THE SOUND PRESSURE FIELD EMITTED BY STATIONARY OR MOVING JETS --; JET NOISE AT VERY LOW AND VERY HIGH SPEED --; AN INVESTIGATION OF THE NEAR NOISE FIELDS OF A CHOKED AXI-SYMMETRIC AIR JET --; NOISE FROM UNDEREXPANDED AXISYMMETRIC JET FLOWS USING RADIAL JET FLOW iMPINGEMENT --; THE RESPONSE OF A SIMPLE PANEL TO THE PSEUDO-SOUND FIELD OF A JET --; ATMOSPHERIC ABSORPTION OF NOISE --; ATTENUATION OF SOUND IN SOFT-WALLED CIRCULAR DUCTS --; FLOW PERTURBATIONS GENERATED BY A SHOCK WAVE INTERACTING WITH AN ENTROPY WAVE --; TRENDS IN BOUNDARY LAYER NOISE RESEARCH --; A REVIEW OF THE SOUND-GENERATING MECHANISMS IN AIRCRAFT-ENGINE FANS AND COMPRESSORS --; A THEORETICAL STUDY OF HELICOPTER ROTOR NOISE --; A STUDY OF PROPELLER NOISE RESEARCH --; REVIEW OF SONIC BOOM THEORY --; RECENT RESULTS OF SONIC BOOM RESEARCH --; SONIC BANG SIMULATION BY EXPLOSIVES --; SECOND-ORDER WAVE STRUCTURE: PLANAR FLOWS --; LIFTING AERODYNAMIC CONFIGURATIONS WITH NO SONIC BOOM
• Format: Mode of access: Internet via World Wide Web.
• ISBN: 9781487582869; 9783110490947
• DOI: 10.3138/9781487582869
• Access: restricted access
• Hierarchical level: Monograph
• Statement of Responsibility: ed. by H.S. Ribner.

The growth of aviation and the increasing size and power of aircraft has made aerodynamic noise a major problem for society. In some places the noise has increased beyond the limits of human tolerance. The problem is not new, but because of its complexity not much has been done about it. Some would argue that the increase in noise is an inevitable by-product of the growth of aviation. Control of this noise will only be possible when more is known of its generation, propagation, and attenuation. To aid in the understanding of the complex problem, the United States Air Force Office of Scientific Research and the Institute for Aerospace Studies, University of Toronto jointly sponsored a symposium on aerodynamic noise in Toronto, May 20-21, 1968, aimed at people involved in research. Papers were invited on the theoretical and practical aspects of noise associated with air flow. Twenty-two of the papers presented are collected here for the use of researchers and engineers concern with aeroacoustics. Chairman of the symposium was Dr. H.S. Ribner, Professor at the University of Toronto Institute of Aerospace Studies, who edited the volume