The Computation And Analysis Of Helicopter Impulsive Noise

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The Computation and Analysis of Helicopter Impulsive Noise

Author	: Xue Yu
Publisher	:
Total Pages	: 346
Release	: 1994
ISBN-10	: MINN:31951D01086990E
ISBN-13	:
Rating	: 4/5 ( Downloads)

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Book Synopsis The Computation and Analysis of Helicopter Impulsive Noise by : Xue Yu

Download or read book The Computation and Analysis of Helicopter Impulsive Noise written by Xue Yu and published by . This book was released on 1994 with total page 346 pages. Available in PDF, EPUB and Kindle. Book excerpt:

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Language: en
Pages: 346

The Computation and Analysis of Helicopter Impulsive Noise

Authors: Xue Yu

Categories:

Type: BOOK - Published: 1994 - Publisher:

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Pages: 18

New Computational Methods for the Prediction and Analysis of Helicopter Noise

Authors: Roger C. Strawn

Categories: Fluid dynamics

Type: BOOK - Published: 1996 - Publisher:

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Abstract: "This paper describes several new methods to predict and analyze rotorcraft noise. These methods are: 1) a combined computational fluid dynamics and K

Language: en
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Helicopter Impulsive Noise: Theoretical and Experimental Status

Authors: F. H. Schmitz

Categories:

Type: BOOK - Published: 1983 - Publisher:

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The theoretical and experimental status of helicopter impulsive noise is reviewed. The two major source mechanisms of helicopter impulsive noise are addressed:

Language: en
Pages: 244

An Experimental Study of Helicopter Rotor Impulsive Noise

Authors: William E. Bausch

Categories:

Type: BOOK - Published: 1971 - Publisher:

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Results of a study of helicopter rotor impulsive noise (RIN) are presented. Rotor noise, together with rotor blade dynamic and pressure data, was measured durin

Language: en
Pages: 30

Comparison of Measured and Calculated Helicopter Rotor Impulsive Noise. [wind Tunnel Test Data and Prediction Analysis Techniques]

Authors: National Aeronautics and Space Administration (NASA)

Categories:

Type: BOOK - Published: 2018-07-26 - Publisher: Createspace Independent Publishing Platform

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The thickness noise theory is discussed. Two full-scale rotors were tested in a wind tunnel with several tips involving changes in chord, thickness, and sweep.