2,196 research outputs found

    The cost of applying current helicopter external noise reduction methods while maintaining realistic vehicle performance

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    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. These methods were 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 hovering ceiling, forward flight range/speed/payload, and rotor stall margin. The results indicate that small, but meaningful, reductions in helicopter noise can be obtained by treating the turbine engine exhaust duct. Furthermore, these reductions do not result in excessive life cycle cost penalties. Currently available main rotor noise reduction methodology, however, is shown to be inadequate and excessively costly

    An analytical method for designing low noise helicopter transmissions

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    The development and experimental validation of a method for analytically modeling the noise mechanism in the helicopter geared power transmission systems is described. This method can be used within the design process to predict interior noise levels and to investigate the noise reducing potential of alternative transmission design details. Examples are discussed

    Probabilistic Risk Analysis and Margin Process for a Flexible Thermal Protection System

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    Atmospheric entry vehicle thermal protection systems are margined due to the uncertainties that exist in entry aeroheating environments and the thermal response of the materials and structures. Entry vehicle thermal protections systems are traditionally over-margined for the heat loads that are experienced along the entry trajectory by designing to survive stacked worst-case scenarios. Additionally, the conventional heat shield design and margin process offers very little insight into the risk of over-temperature during flight and the corresponding reliability of the heat shield performance. A probabilistic margin process can be used to appropriately margin the thermal protection system based on rigorously calculated risk of failure. This probabilistic margin process allows engineers to make informed aeroshell design, entry-trajectory design, and risk trades while preventing excessive margin from being applied. This study presents the methods of the probabilistic margin process and how the uncertainty analysis is used to determine the reliability of the entry vehicle thermal protection system and associated risks of failure

    Nancy Rhoden: Bridging the Disciplines of Law, Medicine, and Ethics

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    The role of antibiotics in the prevention of preterm birth

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    There are multiple uses for antibiotics during pregnancy: treatment of intercurrent bacterial infections such as urinary or respiratory tract infections, maternal treatment to prevent fetal or neonatal disease, prophylactic treatment for surgical procedures, and treatment of puerperal infections. This report will summarize the current recommendations for the use of antibiotics specifically to reduce the risk of preterm birth

    日本の陶芸;第1巻

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    日本の陶芸

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