A Method of Performance Reduction for Helicopters

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis A Method of Performance Reduction for Helicopters by : F. O'Hara

Download or read book A Method of Performance Reduction for Helicopters written by F. O'Hara and published by . This book was released on 1947 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Performance

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Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (113 download)

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Book Synopsis Performance by :

Download or read book Performance written by and published by . This book was released on 1969 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Helicopter Noise Reduction Design Trade-Off Study

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Publisher :
ISBN 13 :
Total Pages : 256 pages
Book Rating : 4.:/5 (227 download)

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Book Synopsis Helicopter Noise Reduction Design Trade-Off Study by : Michael A. Bowes

Download or read book Helicopter Noise Reduction Design Trade-Off Study written by Michael A. Bowes and published by . This book was released on 1977 with total page 256 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study was performed to determine the noise reduction benefits and economic costs associated with applying state-of-the-art noise reduction methods to future design civil helicopters. As part of this study, a survey of the make-up of the civil fleet was performed, and this fleet make-up was projected to the 1980 time frame. Analytical methods were developed and/or adopted for calculating helicopter component noise, and these methods were incorporated into a unified total vehicle noise calculation model. Analytical methods were also developed for calculating the effects of noise reduction methodology on helicopter design, performance and cost. The analytical methods were used to calculate baseline noise and cost characteristics of several existing civil helicopters. These methods were also used to calculate changes in noise, design, performance and cost due to the incorporation of engine and main rotor noise reduction methods. All noise reduction techniques were evaluated in the context of an established mission performance criterion which included consideration of hover ceiling, forward flight range/speed/payload and rotor stall margin.

A Note on the Calculation of Helicopter Performance at High Tip-speed Ratios

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Publisher :
ISBN 13 :
Total Pages : 18 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis A Note on the Calculation of Helicopter Performance at High Tip-speed Ratios by : Alfred Gessow

Download or read book A Note on the Calculation of Helicopter Performance at High Tip-speed Ratios written by Alfred Gessow and published by . This book was released on 1959 with total page 18 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Technical Report

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Publisher :
ISBN 13 :
Total Pages : 1054 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Technical Report by : Aeronautical Research Council (Great Britain)

Download or read book Technical Report written by Aeronautical Research Council (Great Britain) and published by . This book was released on 1959 with total page 1054 pages. Available in PDF, EPUB and Kindle. Book excerpt: Includes its Reports, which are also issued separately.

Research Abstracts

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ISBN 13 :
Total Pages : 568 pages
Book Rating : 4.3/5 ( download)

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Book Synopsis Research Abstracts by : United States. National Advisory Committee for Aeronautics

Download or read book Research Abstracts written by United States. National Advisory Committee for Aeronautics and published by . This book was released on 1951 with total page 568 pages. Available in PDF, EPUB and Kindle. Book excerpt:

A Method for Computing Forward Flight Performance of a Helicopter

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Publisher :
ISBN 13 :
Total Pages : 122 pages
Book Rating : 4.:/5 (522 download)

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Book Synopsis A Method for Computing Forward Flight Performance of a Helicopter by : Charles Howard Armbruster

Download or read book A Method for Computing Forward Flight Performance of a Helicopter written by Charles Howard Armbruster and published by . This book was released on 1952 with total page 122 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Helicopter Test and Evaluation

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Publisher : John Wiley & Sons
ISBN 13 : 1405172541
Total Pages : 384 pages
Book Rating : 4.4/5 (51 download)

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Book Synopsis Helicopter Test and Evaluation by : Alastair Cooke

Download or read book Helicopter Test and Evaluation written by Alastair Cooke and published by John Wiley & Sons. This book was released on 2009-02-12 with total page 384 pages. Available in PDF, EPUB and Kindle. Book excerpt: Although a number of texts on helicopter aerodynamics have been written, few have explained how the various theories concerning rotorborne flight underpin practical flight test and evaluation. This book combines theoretical information on aerodynamics, stability, control and performance with details of evaluation methodologies and practical guidance on the conduct of helicopter flight tests. For each topic the relevant theory is explained briefly and followed by details of the practical aspects of testing a conventional helicopter. These include: * safety considerations * planning the tests * the most efficient way to conduct individual flights Where possible typical test results are presented and discussed. The book draws on the authors' extensive experience in flight test and flight test training and will appeal not only to professionals working in the area of rotorcraft test and evaluation, but also to helicopter pilots, rotorcraft designers and manufacturers and final year undergraduates of aeronautical engineering

Scientific and Technical Aerospace Reports

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Publisher :
ISBN 13 :
Total Pages : 456 pages
Book Rating : 4.:/5 (31 download)

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Book Synopsis Scientific and Technical Aerospace Reports by :

Download or read book Scientific and Technical Aerospace Reports written by and published by . This book was released on 1995 with total page 456 pages. Available in PDF, EPUB and Kindle. Book excerpt: Lists citations with abstracts for aerospace related reports obtained from world wide sources and announces documents that have recently been entered into the NASA Scientific and Technical Information Database.

Performance reduction for ramjet-helicopters

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Publisher :
ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (841 download)

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Book Synopsis Performance reduction for ramjet-helicopters by : F.J. Sterk

Download or read book Performance reduction for ramjet-helicopters written by F.J. Sterk and published by . This book was released on 1961 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Applied Mechanics Reviews

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Publisher :
ISBN 13 :
Total Pages : 616 pages
Book Rating : 4.:/5 (26 download)

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Book Synopsis Applied Mechanics Reviews by :

Download or read book Applied Mechanics Reviews written by and published by . This book was released on 1948 with total page 616 pages. Available in PDF, EPUB and Kindle. Book excerpt:

Revolutionary Concepts for Helicopter Noise Reduction: Silent Program

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Publisher : Independently Published
ISBN 13 : 9781723974304
Total Pages : 90 pages
Book Rating : 4.9/5 (743 download)

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Book Synopsis Revolutionary Concepts for Helicopter Noise Reduction: Silent Program by : National Aeronautics and Space Adm Nasa

Download or read book Revolutionary Concepts for Helicopter Noise Reduction: Silent Program written by National Aeronautics and Space Adm Nasa and published by Independently Published. This book was released on 2018-09-24 with total page 90 pages. Available in PDF, EPUB and Kindle. Book excerpt: As part of a NASA initiative to reduce helicopter main rotor noise, a Phase 1 study has been performed of candidate noise reduction concepts. Both conventional and novel design technologies have been analyzed that reduce the community impact of helicopter operations. In this study the noise reduction potential and design implications are assessed for conventional means of noise reduction, e.g., tip speed reduction, tip shapes and airfoil tailoring, and for two innovative design concepts: modulated blade spacing and x-force control. Main rotor designs that incorporate modulated blade spacing are shown to have reduced peak noise levels in most flight operations. X-force control alters the helicopter's force balance whereby the miss distance between main rotor blades and shed vortices can be controlled. This control provides a high potential to mitigate BVI noise radiation. Each concept is evaluated using best practice design and analysis methods, achieving the study's aim to significantly reduce noise with minimal performance degradation and no vibration increase. It is concluded that a SILENT main rotor design, incorporating the modulated blade spacing concept, offers significantly reduced noise levels and the potential of a breakthrough in how a helicopter's sound is perceived and judged. The SILENT rotor represents a definite advancement in the state-of-the-art and is selected as the design concept for demonstration in Phase 2. A Phase 2 Implementation Plan is developed for whirl cage and wind tunnel evaluations of a scaled model SILENT rotor.Edwards, Bryan and Cox, Charles and Booth, Earl R., Jr. (Technical Monitor)Langley Research CenterAIRCRAFT NOISE; NOISE REDUCTION; NASA PROGRAMS; ROTARY WING AIRCRAFT; AEROACOUSTICS; SOUND WAVES; WAVEFORMS; VORTICES; WIND TUNNELS; AIRFOILS; BLADE-VORTEX INTERACTION

Quality Control, Robust Design, and the Taguchi Method

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Publisher : Springer Science & Business Media
ISBN 13 : 1468414720
Total Pages : 287 pages
Book Rating : 4.4/5 (684 download)

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Book Synopsis Quality Control, Robust Design, and the Taguchi Method by : Khosrow Dehnad

Download or read book Quality Control, Robust Design, and the Taguchi Method written by Khosrow Dehnad and published by Springer Science & Business Media. This book was released on 2012-12-06 with total page 287 pages. Available in PDF, EPUB and Kindle. Book excerpt: In 1980, I received a grant from Aoyama-gakuin university to come to the United States to assist American Industry improve the quality of their products. In a small way this was to repay the help the US had given Japan after the war. In the summer of 1980, I visited the AT&T Bell Laboratories Quality Assurance Center, the organization that founded modern quality control. The result of my first summer at AT&T was an experiment with an orthogonal array design of size 18 (OA18) for optimization of an LSI fabrication process. As a measure of quality, the quantity "signal-ta-noise" ratio was to be optimized. Since then, this experi mental approach has been named "robust design" and has attracted the attention of both engineers and statisticians. My colleagues at Bell Laboratories have written several expository articles and a few theoretical papers on robust design from the viewpoint of statistics. Because so many people have asked for copies of these papers, it has been decided to publish them in a book form. This anthology is the result of these efforts. Despite the fact that quality engineering borrows some technical words from traditional design of experiments, the goals of quality engineering are different from those of statistics. For example, suppose there are two vendors. One vendor supplies products whose quality characteristic has a normal distribution with the mean on target (the desired value) and a certain standard deviation.

An Experimental Investigation Into the Performance of a Helicopter Following Sudden Reduction in Power

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ISBN 13 :
Total Pages : pages
Book Rating : 4.:/5 (11 download)

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Book Synopsis An Experimental Investigation Into the Performance of a Helicopter Following Sudden Reduction in Power by : G. F. Langdon

Download or read book An Experimental Investigation Into the Performance of a Helicopter Following Sudden Reduction in Power written by G. F. Langdon and published by . This book was released on 1955 with total page pages. Available in PDF, EPUB and Kindle. Book excerpt:

Basic Helicopter Handbook

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ISBN 13 :
Total Pages : 124 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis Basic Helicopter Handbook by : United States. Flight Standards Service

Download or read book Basic Helicopter Handbook written by United States. Flight Standards Service and published by . This book was released on 1973 with total page 124 pages. Available in PDF, EPUB and Kindle. Book excerpt:

An Analysis of the Autorotative Performance of a Helicopter Powered by Rotor-tip Jet Units

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Publisher :
ISBN 13 :
Total Pages : 36 pages
Book Rating : 4.3/5 (91 download)

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Book Synopsis An Analysis of the Autorotative Performance of a Helicopter Powered by Rotor-tip Jet Units by : Alfred Gessow

Download or read book An Analysis of the Autorotative Performance of a Helicopter Powered by Rotor-tip Jet Units written by Alfred Gessow and published by . This book was released on 1950 with total page 36 pages. Available in PDF, EPUB and Kindle. Book excerpt: A study of the autorotative performance of an assumed helicopter powered by jet units located at the rotor tips is presented. It is concluded that the power-off drag of tip jet units could cause a marked and perhaps dangerous increase in the minimum rate of descent of the helicopter unless steps are take to reduce the power-off drag of the units.

Principles of Helicopter Aerodynamics with CD Extra

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Publisher : Cambridge University Press
ISBN 13 : 9780521858601
Total Pages : 860 pages
Book Rating : 4.8/5 (586 download)

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Book Synopsis Principles of Helicopter Aerodynamics with CD Extra by : Gordon J. Leishman

Download or read book Principles of Helicopter Aerodynamics with CD Extra written by Gordon J. Leishman and published by Cambridge University Press. This book was released on 2006-04-24 with total page 860 pages. Available in PDF, EPUB and Kindle. Book excerpt: Written by an internationally recognized teacher and researcher, this book provides a thorough, modern treatment of the aerodynamic principles of helicopters and other rotating-wing vertical lift aircraft such as tilt rotors and autogiros. The text begins with a unique technical history of helicopter flight, and then covers basic methods of rotor aerodynamic analysis, and related issues associated with the performance of the helicopter and its aerodynamic design. It goes on to cover more advanced topics in helicopter aerodynamics, including airfoil flows, unsteady aerodynamics, dynamic stall, and rotor wakes, and rotor-airframe aerodynamic interactions, with final chapters on autogiros and advanced methods of helicopter aerodynamic analysis. Extensively illustrated throughout, each chapter includes a set of homework problems. Advanced undergraduate and graduate students, practising engineers, and researchers will welcome this thoroughly revised and updated text on rotating-wing aerodynamics.