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 exi...
Nowadays helicopters play a pivotal role in a wide variety of activities from important military mis...
External and internal aircraft noise requirements are discussed in terms of application to military ...
PDFTech ReportFAA-RD-77-57, 1HelicoptersAircraft noiseDatabasesGround effectApproachGlide path syste...
Analytical methods were developed and/or adopted for calculating helicopter component noise, and the...
November 1971Includes bibliographical references (p. 52)The relationship between noise reduction and...
A means of estimating the noise generated by a helicopter main rotor using information which is gene...
A review of helicopter noise measurement programs and noise reduction/economic studies of FAA is giv...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
The interior noise levels of existing helicopters are discussed along with an ongoing experimental p...
1986PDFTech ReportFAA-EE-86-01HelicoptersHeliportsAircraft noiseAirport noiseEnvironmental impactsSt...
A field noise measurement program has been conducted on a standard OH-6A helicopter and one that had...
The establishment of a realistic plan for NASA and the U.S. helicopter industry to develop a design-...
August 1974Includes bibliographical references (p. 48-50)The relationship between direct operating c...
As part of a NASA initiative to reduce helicopter main rotor noise, a Phase 1 study has been perform...
February 1976Includes bibliographical references (p. 50-51)The relationship between direct operating...
Nowadays helicopters play a pivotal role in a wide variety of activities from important military mis...
External and internal aircraft noise requirements are discussed in terms of application to military ...
PDFTech ReportFAA-RD-77-57, 1HelicoptersAircraft noiseDatabasesGround effectApproachGlide path syste...
Analytical methods were developed and/or adopted for calculating helicopter component noise, and the...
November 1971Includes bibliographical references (p. 52)The relationship between noise reduction and...
A means of estimating the noise generated by a helicopter main rotor using information which is gene...
A review of helicopter noise measurement programs and noise reduction/economic studies of FAA is giv...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
The interior noise levels of existing helicopters are discussed along with an ongoing experimental p...
1986PDFTech ReportFAA-EE-86-01HelicoptersHeliportsAircraft noiseAirport noiseEnvironmental impactsSt...
A field noise measurement program has been conducted on a standard OH-6A helicopter and one that had...
The establishment of a realistic plan for NASA and the U.S. helicopter industry to develop a design-...
August 1974Includes bibliographical references (p. 48-50)The relationship between direct operating c...
As part of a NASA initiative to reduce helicopter main rotor noise, a Phase 1 study has been perform...
February 1976Includes bibliographical references (p. 50-51)The relationship between direct operating...
Nowadays helicopters play a pivotal role in a wide variety of activities from important military mis...
External and internal aircraft noise requirements are discussed in terms of application to military ...
PDFTech ReportFAA-RD-77-57, 1HelicoptersAircraft noiseDatabasesGround effectApproachGlide path syste...