A study was conducted to forecast the noise restrictions which may be imposed on civil transport helicopters in the 1975-1985 time period. Certification and community acceptance criteria were predicted. A 50 passenger tandem rotor helicopter based on the Boeing-Vertol Model 347 was studied to determine the noise reductions required, and the means of achieving them. Some of the important study recommendations are: (1) certification limits should be equivalent to 95 EPNdb at data points located at 500 feet to each side of the touchdown/takeoff point, and 1000 feet from this point directly under the approach and departure flight path. (2) community acceptance should be measured as Equivalent Noise Level (Leq), based on dBA, with separate limit...
A broad perspective of needs in helicopter exterior and interior control is presented. Emphasis is g...
Machine learning techniques are applied to the NASA Langley Research Center's expansive database of ...
The interior noise levels of existing helicopters are discussed along with an ongoing experimental p...
A study was conducted to define those criteria necessary for civil helicopter operations to be acous...
A review of helicopter noise measurement programs and noise reduction/economic studies of FAA is giv...
1986PDFTech ReportFAA-EE-86-01HelicoptersHeliportsAircraft noiseAirport noiseEnvironmental impactsSt...
Enactment of helicopter noise certification standards for the control of noise impact contributing t...
Exterior and interior noise problems are addressed both from the physics and engineering as well as ...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
PDFTech ReportFAA-RD-77-57, 1HelicoptersAircraft noiseDatabasesGround effectApproachGlide path syste...
A computationally efficient, semiempirical noise model suitable for maneuvering flight noise predict...
The establishment of a realistic plan for NASA and the U.S. helicopter industry to develop a design-...
A field noise measurement program has been conducted on a standard OH-6A helicopter and one that had...
Calculated engine core noise levels, based on NASA-Lewis prediction procedures, for five representat...
Analytical methods were developed and/or adopted for calculating helicopter component noise, and the...
A broad perspective of needs in helicopter exterior and interior control is presented. Emphasis is g...
Machine learning techniques are applied to the NASA Langley Research Center's expansive database of ...
The interior noise levels of existing helicopters are discussed along with an ongoing experimental p...
A study was conducted to define those criteria necessary for civil helicopter operations to be acous...
A review of helicopter noise measurement programs and noise reduction/economic studies of FAA is giv...
1986PDFTech ReportFAA-EE-86-01HelicoptersHeliportsAircraft noiseAirport noiseEnvironmental impactsSt...
Enactment of helicopter noise certification standards for the control of noise impact contributing t...
Exterior and interior noise problems are addressed both from the physics and engineering as well as ...
A field noise measurement program has been conducted using both a standard SH-3A helicopter and an S...
PDFTech ReportFAA-RD-77-57, 1HelicoptersAircraft noiseDatabasesGround effectApproachGlide path syste...
A computationally efficient, semiempirical noise model suitable for maneuvering flight noise predict...
The establishment of a realistic plan for NASA and the U.S. helicopter industry to develop a design-...
A field noise measurement program has been conducted on a standard OH-6A helicopter and one that had...
Calculated engine core noise levels, based on NASA-Lewis prediction procedures, for five representat...
Analytical methods were developed and/or adopted for calculating helicopter component noise, and the...
A broad perspective of needs in helicopter exterior and interior control is presented. Emphasis is g...
Machine learning techniques are applied to the NASA Langley Research Center's expansive database of ...
The interior noise levels of existing helicopters are discussed along with an ongoing experimental p...