1,412 research outputs found

    Gender Difference in Preference and Prejudice for Female Body Shapes

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    Research shows that overweight individuals face prejudice, but there is no research whether that a specific body type faces more or less prejudice. In the four main female body shapes- Apple, Banana, Pear, and Hourglass, fat is distributed differently. The purpose of this study is to examine gender differences in preference, idealization, and prejudice patterns for female body types amongst undergraduates. Participants were presented with four body shapes and asked to give 1) their preference, 2) their prediction of the opposite sex’s preference, and 3) their ideal body type. Then the particpants selected four adjectives to attribute to each body shape from a preselected pool of negative and positive adjectives. Results from this study supported previous research on hip-to-waist ratio and body type negative and positive attribute association

    Evaluating and Enabling Scalable High Performance Computing Workloads on Commercial Clouds

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    Performance, usability, and accessibility are critical components of high performance computing (HPC). Usability and performance are especially important to academic researchers as they generally have little time to learn a new technology and demand a certain type of performance in order to ensure the quality and quantity of their research results. We have observed that while not all workloads run well in the cloud, some workloads perform well. We have also observed that although commercial cloud adoption by industry has been growing at a rapid pace, its use by academic researchers has not grown as quickly. We aim to help close this gap and enable researchers to utilize the commercial cloud more efficiently and effectively. We present our results on architecting and benchmarking an HPC environment on Amazon Web Services (AWS) where we observe that there are particular types of applications that are and are not suited for the commercial cloud. Then, we present our results on architecting and building a provisioning and workflow management tool (PAW), where we developed an application that enables a user to launch an HPC environment in the cloud, execute a customizable workflow, and after the workflow has completed delete the HPC environment automatically. We then present our results on the scalability of PAW and the commercial cloud for compute intensive workloads by deploying a 1.1 million vCPU cluster. We then discuss our research into the feasibility of utilizing commercial cloud infrastructure to help tackle the large spikes and data-intensive characteristics of Transportation Cyberphysical Systems (TCPS) workloads. Then, we present our research in utilizing the commercial cloud for urgent HPC applications by deploying a 1.5 million vCPU cluster to process 211TB of traffic video data to be utilized by first responders during an evacuation situation. Lastly, we present the contributions and conclusions drawn from this work

    Vernal Conjunctivitis.

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    The Cauchy-Schlomilch transformation

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    The Cauchy-Schl\"omilch transformation states that for a function ff and a, b>0a, \, b > 0, the integral of f(x2)f(x^{2}) and af((ax−bx−1)2af((ax-bx^{-1})^{2} over the interval [0,∞)[0, \infty) are the same. This elementary result is used to evaluate many non-elementary definite integrals, most of which cannot be obtained by symbolic packages. Applications to probability distributions is also given

    The Low-Noise Potential of Distributed Propulsion on a Catamaran Aircraft

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    The noise shielding potential of an inboard-wing catamaran aircraft when coupled with distributed propulsion is examined. Here, only low-frequency jet noise from mid-wing-mounted engines is considered. Because low frequencies are the most difficult to shield, these calculations put a lower bound on the potential shielding benefit. In this proof-of-concept study, simple physical models are used to describe the 3-D scattering of jet noise by conceptualized catamaran aircraft. The Fast Scattering Code is used to predict noise levels on and about the aircraft. Shielding results are presented for several catamaran type geometries and simple noise source configurations representative of distributed propulsion radiation. Computational analyses are presented that demonstrate the shielding benefits of distributed propulsion and of increasing the width of the inboard wing. Also, sample calculations using the FSC are presented that demonstrate additional noise reduction on the aircraft fuselage by the use of acoustic liners on the inboard wing trailing edge. A full conceptual aircraft design would have to be analyzed over a complete mission to more accurately quantify community noise levels and aircraft performance, but the present shielding calculations show that a large acoustic benefit could be achieved by combining distributed propulsion and liner technology with a twin-fuselage planform
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