2,994 research outputs found
An engineering study of hybrid adaptation of wind tunnel walls for three-dimensional testing
Solid wall tunnels having only upper and lower walls flexing are described. An algorithm for selecting the wall contours for both 2 and 3 dimensional wall flexure is presented and numerical experiments are used to validate its applicability to the general test case of 3 dimensional lifting aircraft models in rectangular cross section wind tunnels. The method requires an initial approximate representation of the model flow field at a given lift with wallls absent. The numerical methods utilized are derived by use of Green's source solutions obtained using the method of images; first order linearized flow theory is employed with Prandtl-Glauert compressibility transformations. Equations are derived for the flexed shape of a simple constant thickness plate wall under the influence of a finite number of jacks in an axial row along the plate centerline. The Green's source methods are developed to provide estimations of residual flow distortion (interferences) with measured wall pressures and wall flow inclinations as inputs
Unsteady pressure and structural response measurements of an elastic supercritical wing
Results are presented which define unsteady flow conditions associated with high dynamic response experienced on a high aspect ratio elastic supercritical wing at transonic test conditions while being tested in the NASA Langley Transonic Dynamics Tunnel. The supercritical wing, designed for a cruise Mach number of 0.80, experienced the high dynamic response in the Mach number range from 0.90 to 0.94 with the maximum response occurring at a Mach number of approximately 0.92. At the maximum wing response condition the forcing function appears to be the oscillatory chordwise movement of strong shocks located on both the wing upper and lower surfaces in conjunction with the flow separating and reattaching in the trailing edge region
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Repeatability Analysis of 304L Deposition by the LENS® Process
Sandia National Laboratories is currently engaging in an effort to qualify Laser Engineered Net
Shaping™ (LENS®) as a repair and modification process for high rigor metal components. As
part of that effort, the LENS team has conducted a process repeatability test to help identify
variation within the system. This test utilized 304L stainless steel which is a commonly used
material at Sandia. Over the course of 12 weeks, 3/8”x3/8”x2” towers were built in sets of 3
with a total of 30 towers completed. A random sampling of 10 of these towers (1 from each set
of 3) had been identified before depositing the towers, and these towers were used for tensile
testing and metallographic testing. The testing showed the ultimate and yield strengths of all
samples to be well above those of annealed 304L. This is expected because of the rapid melt
pool solidification present in the LENS process and the resulting grain refinement. The ductility,
which usually remains on par with annealed 304L, was found to be lower. The final cause of this
loss of ductility was determined to be inter-layer separation due to loose wires in the closed loop
melt pool control system.Englis
Environmental justice in the context of sustainable urban renewal / regeneration: the case for heritage at Constitution Hill
Since the birth of democracy in South Africa, Urban Geography has
experienced many paradigmatic and epistemological shifts; within Human
Geography 'planning' faces various challenges in the new Millennium.
Environmental management, in light of the emphasis on sustainable
development, sees many urban planners and politicians strive to reconcile
environmentalism with development that is equitable. The emergence of the
environmental justice discourse is significant, since inter-generational justice
(as enshrined in sustainable development) is a key issue, this research report
used heritage as a lens to explore this complex relationship in regard to
urban regeneration. Using a case study approach this report shows the
nature and context of postmodern urban environmental management.
Special reference to the significance and impact of environmental justice on
the cityscape of Johannesburg is made, as this report suggests that
environmental justice is a useful conceptual framework to give depth and
meaning to sustainable development, in urban regeneration as a policy
objective. The use of Constitution Hill as a case study placed the project in a
post-apartheid South African context
The financial clouds review
This paper demonstrates financial enterprise portability, which involves moving entire application services from desktops to clouds and between different clouds, and is transparent to users who can work as if on their familiar systems. To demonstrate portability, reviews for several financial models are studied, where Monte Carlo Methods (MCM) and Black Scholes Model (BSM) are chosen. A special technique in MCM, Least Square Methods, is used to reduce errors while performing accurate calculations. The coding algorithm for MCM written in MATLAB is explained. Simulations for MCM are performed on different types of Clouds. Benchmark and experimental results are presented for discussion. 3D Black Scholes are used to explain the impacts and added values for risk analysis, and three different scenarios with 3D risk analysis are explained. We also discuss implications for banking and ways to track risks in order to improve accuracy. We have used a conceptual Cloud platform to explain our contributions in Financial Software as a Service (FSaaS) and the IBM Fined Grained Security Framework. Our objective is to demonstrate portability, speed, accuracy and reliability of applications in the clouds, while demonstrating portability for FSaaS and the Cloud Computing Business Framework (CCBF), which is proposed to deal with cloud portability
Investigation of transonic region of high dynamic response encountered on an elastic supercritical wing
Unsteady aerodynamic data were measured on an aspect ratio 10.3 elastic supercritical wing while undergoing high dynamic response above a Mach number of 0.90. These tests were conducted in the NASA Langley Transonic Dynamics Tunnel. A previous test of this wing predicted an unusual instability boundary based on subcritical response data. During the present test no instability was found, but an angle of attack dependent narrow Mach number region of high dynamic wing response was observed over a wide range of dynamic pressures. The effect on dynamic wing response of wing angle of attack, static outbound control surface deflection and a lower surface spanwise fence located near the 60 percent local chordline was investigated. The driving mechanism of the dynamic wing response appears to be related to chordwise shock movement in conjunction with flow separation and reattachment on both the upper and lower surfaces
Investigation and suppression of high dynamic response encountered on an elastic supercritical wing
The DAST Aeroelastic Research Wing had been previously in the NASA Langley TDT and an unusual instability boundary was predicted based upon supercritical response data. Contrary to the predictions, no instability was found during the present test. Instead a region of high dynamic wing response was observed which reached a maximum value between Mach numbers 0.92 and 0.93. The amplitude of the dynamic response increased directly with dynamic pressure. The reponse appears to be related to chordwise shock movement in conjunction with flow separation and reattachment on the upper and lower wing surfaces. The onset of flow separation coincided with the occurrence of strong shocks on a surface. A controller was designed to suppress the wing response. The control law attenuated the response as compared with the uncontrolled case and added a small but significant amount of damping for the lower density condition
Crowd counting using group tracking and local features
In public venues, crowd size is a key indicator of crowd safety and stability. In this paper we propose a crowd counting algorithm that uses tracking and local features to count the number of people in each group as represented by a foreground blob segment, so that the total crowd estimate is the sum of the group sizes. Tracking is employed to improve the robustness of the estimate, by analysing the history of each group, including splitting and merging events. A simplified ground truth annotation strategy results in an approach with minimal setup requirements that is highly accurate
Large scale monitoring of crowds and building utilisation: A new database and distributed approach
Public buildings and large infrastructure are typically monitored by tens or hundreds of cameras, all capturing different physical spaces and observing different types of interactions and behaviours. However to date, in large part due to limited data availability, crowd monitoring and operational surveillance research has focused on single camera scenarios which are not representative of real-world applications. In this paper we present a new, publicly available database for large scale crowd surveillance. Footage from 12 cameras for a full work day covering the main floor of a busy university campus building, including an internal and external foyer, elevator foyers, and the main external approach are provided; alongside annotation for crowd counting (single or multi-camera) and pedestrian flow analysis for 10 and 6 sites respectively. We describe how this large dataset can be used to perform distributed monitoring of building utilisation, and demonstrate the potential of this dataset to understand and learn the relationship between different areas of a building
Geometrical and structural properties of an Aeroelastic Research Wing (ARW-2)
Transonic steady and unsteady pressure tests were conducted on a large elastic wing known as the DAST ARW-2 wing. The wing has a supercritical airfoil, an aspect ratio of 10.3, a leading edge sweepback angle of 28.8 deg and is equipped with two inboard and one outboard trailing edge control surfaces. The geometrical and structural characteristics are presented of this elastic wing, using a combination of measured and calculated data, to permit future analyst to compare the experimental surface pressure data with theoretical predictions
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