Technical Reviewers
Symbols
1.   Propeller and Propfan Noise - B. Magliozzi, D.B. Hanson, and R.K. Amiet
2.   Rotor Noise - F.H. Schmitz
3.   Turbomachinery Noise - John F. Groeneweg, Thomas G. Sofrin, Edward J. Rice,
and Phillip R. Gliebe
4.   Jet Noise Classical Theory and Experiments - G.M. Lilley
5.   Noise From Turbulent Shear Flows - M.E. Goldstein
6.   Jet Noise Generated by Large-Scale Coherent Motion - Christopher K.W.
Tam
7.   Airframe Noise - David G. Crighton
8.   Propulsive Lift Noise - Martin R. Fink
9.   Combustion and Core Noise - J. Robert Mahan and Allen Karchmer
10.   Sonic Boom - Domenic J. Maglieri and Kenneth J. Plotkin
Glossary of Terms
Index
Return to List of Publications
Technical Reviewers
Symbols
11.   Human Response to Aircraft Noise - Clemans A. Powell and James M.
Fields
12.   Atmospheric Propagation - Tony F.W. Embleton and Gilles A. Daigle
13.   Theoretical Models for Duct Acoustic Propagation and Radiation - Walter
Eversman
14.   Design and Performance of Duct Acoustic Treatment - R.E. Motsinger and R.E.
Kraft
15.   Jet Noise Suppression - P.R. Gliebe, J.F. Brausch, R.K. Majjigi, and R. Lee
16.   Interior Noise - John S. Mixson and John F. Wilby
17.   Flyover-Noise Measurement and Prediction - Noel A. Peart, M.J.T. Smith, B.
Magliozzi, Harry Sternfeld, and the Boeing Noise Engineering Organization
18.   Quiet Aircraft Design and Operational Characteristics - Charles G. Hodge
Glossary of Terms
Index
Return to List of Publications
The field of aeroacoustics has matured dramatically in the past two decades. Researchers have
gained significant theoretical and experimental understanding of the noise generated by aircraft
power plants and their components. In addition, airframe noise and interior noise have been
investigated extensively. The physical understanding obtained from these efforts has resulted in
the development of hardware capable of reducing community noise and of meeting strict noise
certification requirements. Reductions in overall sound pressure level of 20 to 30 dB have been
obtained for some types of power plants, while in the same period their installed power has
increased significantly.
Current quiet flight vehicle designs are based on information reported in a multitude of journals,
conference proceedings, research reports, and specialized books. Each of these scientific
publications represents only incremental steps in the evolution of our present understanding of
the various aeroacoustic noise generation and propagation mechanisms and procedures for noise
control. There is thus a need for a reference document summarizing the current status of
aeroacoustics. It is recognized that some other fine books on aeroacoustics are already available.
The reader is referred to the classic handbooks by Harris on noise and vibration control; to
Goldstein's "Aeroacoustics," which provides a general theoretical treatment of most aeroacoustic
noise sources; to the text "Noise and Acoustic Fatigue in Aeronautics" by Richard and Mead;
and to the AIAA Preprint Series volume entitled "Aerodynamic Noise." The current book
represents an attempt to integrate and update the information in previous related publications, to
provide a balanced viewpoint with both fundamental and applied aspects being considered, and
to focus on those topics that are significant for the design and operation of quiet flight vehicles.
In July 1982, the Continuing Education Subcommittee of the Institute of Aeronautics and
Astronautics (AIAA) Aeroacoustics Technical Committee identified a critical need for a
reference book summarizing and interpreting the status of research in aeroacoustics. The full
Aeroacoustics Technical Committee agreed with this conclusion and enthusiastically supported
the concept of publishing such a book. The book would have a scope consistent with that of the
Technical Committee and would include physics of noise produced by motion of fluids and
bodies through the atmosphere and by chemical reaction processes; it would also include the
responses of human beings, structures, and the atmosphere to aerodynamic noise. The
subcommittee was then instructed to prepare an initial outline of the book for planning purposes
and to procure financial support for its printing. This effort has been given generous support by
the Langley, Lewis and Ames Research Centers of the National Aeronautics and Space
Administration (NASA); the U.S. Air Force Wright Research and Development Center; and the
U.S. Army Aviation Systems Command.
This book is planned as a reference publication, easily readable by persons with scientific or
engineering training who have completed a bachelor degree study program. It serves as an
authoritative resource book for teachers, students, and researchers, but it is not designed for use
directly as a textbook. It provides recommended methodology to evaluate aeroacoutics-related
problems and suggests approaches to their solutions, without extensive tables, nomographs, and
derivations. It is oriented toward flight vehicles and emphasizes underlying physical concepts.
Theoretical, experimental, and applied aspects are covered, including the main formulations, and
comparisons of theory and experiment.
The preparation of the material for this book has been carried out under the general supervision
of the AIAA Technical Committee on Aeoracoustics. The Committee elected the editor (Harvey
H. Hubbard), two associate editors (Christopher K.W. Tam and Robert H. Schlinker), and six
additional editors (Charles E. Feiler, James C. Yu, Walter K. Eversman, Marvin E. Goldstein,
Robert E. Kraft, and Yung H. Yu). Donald L. Lansing and John Laufer (until his untimely death)
also served for short terms. They functioned as an editorial board to establish the overall policy
for the organizing reviewing, and editing of the book. Each was selected because of his expert
knowledge of at least one of the specialty areas covered in the book. They collectively comprise
a team of experts who represent industry, government, and academia viewpoints.
The editorial board members chose by vote the lead authors for each chapter based on their
stature and expertise in particular technical areas and on their proven ability to communicate. In
all cases, contributing authors were selected and enlisted by the lead authors and on the basis of
the same criteria. An outline of each chapter was first approved by the editorial board as a means
of defining the overall scope of that chapter. Technical reviewers were chosen by vote of the
editorial board based on their expertise of subject matter and the nature of their experience. Two
to four persons were selected to provide technical reviews for each manuscript. These technical
reviews were then provided to the appropriate authors as a basis for the preparation of their final
manuscripts. Final editing was accomplished by Mary K. McCaskill and Thomas H. Brinkley of
the NASA Langley Research Center Technical Editing Branch. This latter effort involved skilled
technical editors closely associated with the publication profession. Their work included
checking for accuracy, grammar, consistency of style, compliance with editorial instructions, and
assembly for printing.
Authors and reviewers contributed their time for this project without receiving compensation.
Draft manuscript preparation, typing, and graphics were supported partially or wholly by the
participant's employer. All these contributions were vital to the success of this project and are
greatly appreciated.
Supporting reference information cited in this book is limited to publications available at the
time of the text preparation. No proprietary or classified information is included in order to
protect the interests of authors' companies and governments. In order to enhance its utility, this
book is divided into two volumes, each of which has a list of symbols, an index, and a separate
glossary of terms. Reference lists for each chapter contain the key available supporting
documents.
Volume 1 includes all the chapters that relate directly to the sources of flight vehicle noise:
Propeller and Propfan Noise; Rotor Noise; Turbomachinery Noise; Jet Noise Classical Theory
and Experiments; Noise From Turbulent Shear Flows; Lift Noise; Combustion and Core Noise;
and Sonic Boom. Volume 2 includes those chapters that relate to flight vehicle noise control
and/or operations: Human Response to Aircraft Noise; Atmospheric Propagation; Theoretical
Models for Duct Acoustic Propagation and Radiation; Design and Performance of Duct Acoustic
Treatment; Jet Noise Suppression; Interior Noise; Flyover-Noise Measurement and Prediction;
and Quiet Aircraft Design and Operational Characteristics.
This book was published initially in August 1991 as NASA Reference Publication 1258, Vols. 1
and 2, and with a companion United States Air Force Wright Research and Development Center
designation as Technical Report 90-3052, Vols. 1 and 2. It was printed in soft cover and carried
the appropriate NASA, U.S. Air Force, and U.S. Army logos on its covers.
In November 1993, the Acoustical Society of America agreed to reprint it in a hard-cover version
but with modifications to the covers and title pages and with minor changes and corrections to
the text. Elaine Moran of the Acoustical Society of America and Andrew Prince of the American
Institute of Physics have coordinated the preparation of materials for this reprinting.
VOLUME 1 CONTENTS
CONTENTS Volume 2
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