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Showing papers by "Vaughn College of Aeronautics and Technology published in 2003"


Journal ArticleDOI
TL;DR: In this article, the authors used Monte Carlo simulations to estimate the detection efficiency of microlensing event detection efficiency, where they constructed the I-band extinction map of their GB fields in order to find dereddened magnitudes.
Abstract: We analyze the data of the gravitational microlensing survey carried out by the Microlensing Observations in Astrophysics (MOA) group during 2000 toward the Galactic bulge (GB). Our observations are designed to detect efficient high-magnification events with faint source stars and short-timescale events, by increasing the sampling rate up to ~6 times per night and using Difference Image Analysis (DIA). We detect 28 microlensing candidates in 12 GB fields corresponding to 16 deg2. We use Monte Carlo simulations to estimate our microlensing event detection efficiency, where we construct the I-band extinction map of our GB fields in order to find dereddened magnitudes. We find a systematic bias and large uncertainty in the measured value of the timescale tE,out in our simulations. They are associated with blending and unresolved sources, and are allowed for in our measurements. We compute an optical depth τ = 2.59 × 10-6 toward the GB for events with timescales 0.3 10). These events are useful for studies of extrasolar planets.

210 citations


Journal ArticleDOI
TL;DR: In this article, the authors present the modeling and simulation of the residual stress field resulting from the shot peening process and show that a significant decrease of welding induced tensile residual stress magnitude can be obtained.

98 citations


Journal ArticleDOI
TL;DR: In this paper, the impact and penetration damage of a composite aircraft sandwich panel by a solid, round-shaped impactor is analyzed using finite element analysis codes, and good agreement was obtained between numerical and experimental results, in particular, the numerical simulation was able to predict impact damage and impact energy absorbed by the structure.

93 citations


Journal ArticleDOI
TL;DR: In this paper, the use of cold expansion process as a life extension technique on aircraft structural joints was investigated and the results indicate that significant life improvements can be obtained through cold expansion applied at all percentages of fatigue life tested in this work with the optimum stage being around 25% of the baseline life.

50 citations


Journal ArticleDOI
TL;DR: This paper will focus on the development of an innovative method for estimating odour fluxes and the contributing source areas from a Municipal Solid Waste (MSW) landfill site using a micrometeorological model based on the estimation of footprints of scalar odour concentration measurements in the atmospheric surface layer.
Abstract: This paper will focus on the development of an innovative method for estimating odour fluxes and the contributing source areas from a Municipal Solid Waste (MSW) landfill site. A micrometeorological model has been developed based on the estimation of footprints of scalar odour concentration measurements in the atmospheric surface layer. The model is based on an analytical solution of the Eulerian advection-diffusion equation for vertical diffusion; model parameters include the location of the odour sensor and standard surface layer scaling factors. Lindvall Hoods are commonly used for measuring odour fluxes from ground based fugitive sources. However these cannot replicate the real atmospheric conditions. Common micrometeorological techniques for determining fluxes, such as vertical gradient measurements or eddy correlation methods, yield a flux magnitude but give practically no information about the source location. On the other hand the flux footprint describes the expansion and contraction of the required fetch under varying atmospheric stabilities. Preliminary results from the model are quite encouraging and agree well with those from Lindvall hood measurements. The accuracy of Lindvall hood measurements depends on how tightly the hood is positioned on the uneven landfill surface. It should prevent any air escaping out from the sides of the hood open to the atmosphere. Typical results show an average odour flux of ±25.91 (ou m−2 s−1) from freshly tipped wastes for an upwind fetch of 45.0 m and with the sensor at a height of 1.5 m from the ground. The hood results have a geometric mean of ±29.35 (ou m−2 s−1) based on the inlet air volume and a shade air temperature of 22.5 °C.

31 citations



Journal ArticleDOI
TL;DR: In this paper, the capability of four closed-form solutions for calculating cold expansion-induced residual stresses for three aerospace grade aluminium alloys of medium thickness was investigated, and it was shown that good prediction of crack growth life can be obtained if a suitable closed form model is used.

29 citations


Journal ArticleDOI
TL;DR: In this paper, the authors focused on the calculation of the cost of equity capital in a sample of airlines, in comparison to industry-calculated values, and found that the calculated β values are sensitive to the precise methodology and calculations used.

29 citations


Journal ArticleDOI
TL;DR: In this article, composite films consisting of nanoscale Au particles uniformly embedded in barium titanate (BaTiO 3 ) matrices were prepared by alternate ablation of metallic Au and ceramic BaTiO3 targets using pulsed laser deposition (PLD) technique.

13 citations


Journal ArticleDOI
TL;DR: In this article, the authors describe the research into the flight dynamics modelling and flight control of a flapping wing micro aerial vehicle (MAV) using MATLAB and SIMULINK.
Abstract: This paper describes the research into the flight dynamics modelling and flight control of a flapping wing micro aerial vehicle (MAV). The equations of motion based on a multi-body representation of the vehicle and the flapping wings were derived and form the basis for the simulation program, which was developed using MATLAB and SIMULINK. The aerodynamic forces were obtained through experimental methods and form the basis for the aerodynamic model. The hovering and low speed flight of the MAV was investigated using a SIMULINK simulation model. Various flight control concepts, inspired by observation of insect and bird flight, were investigated in some detail. The concepts include the control of flap frequency, flap and pitch phasing (wing beat kinematics) and shift in centre of gravity position. The paper concludes with a comparison of the control concepts and their feasibility for a practical vehicle application.

8 citations


Journal ArticleDOI
TL;DR: In this paper, the influence of source terms that include losses of momentum and energy is explored and some lessons to be learnt about the physics of multiphase flows from the present theory, but its primary value is via the provision of test problems for numerical methods in the presence of sources.