Now showing items 87-106 of 182

    • Identifying elastic wave polarization and bandgaps in periodic solid media 

      Carrillo-Munoz, Maria; Sharma, Bhisham N. (Elsevier Ltd, 2023-08-15)
      We present a new computational method to accurately identify the elastic wave propagation modes and polarizations in periodic solid structures and metamaterials. The method uses the eigenvectors associated with each ...
    • Impact of launch injection error on orbit-raising of all-electric satellites 

      Bascue, Nikolas; Dutta, Atri; Ghosh, Pradipto (American Institute of Aeronautics and Astronautics Inc, 2020-01-05)
      The effect of launch injection errors on the deployment time and deployed mass of all-electric satellites is investigated in this paper. A stochastic formulation is presented to capture the effect of uncertainties in the ...
    • In-plane shear response of a composite hexagonal honeycomb core under large deformation – A numerical and experimental study 

      Shahverdi Moghaddam, Hooman; Keshavanarayana, Suresh R.; Ivanov, Dmitry S.; Yang, Chihdar Charles; Horner, Allison L. (Elsevier, 2021-07-15)
      In the present work, experimental shear tests using a custom-built picture-frame shear fixture have been conducted to investigate the in-plane pure-shear response of an HRP-C fiberglass/phenolic hexagonal honeycomb core ...
    • In-plane thermal characterization of fiberglass/phenolic honeycomb core through an experimental-numerical approach 

      Shahverdi Moghaddam, Hooman; Keshavanarayana, Suresh R.; Kothare, Aakash; Teoh, Ping; Yang, Chihdar Charles; Horner, Allison L. (DEStech Publications Inc., 2018)
      In the present study, a series of in-plane quasi-static tensile and compressive tests are carried out on a commercial Fiberglass/Phenolic hexagonal cell honeycomb core at elevated temperatures to investigate the high ...
    • Incorporation of physics-based machining models in real-time decision making via metamodels 

      Sharma, Bhisham N.; Harikrishnan, Rishab V.; McCrorie, Stuart B.; Conner, Marc C.; Salahshoor, Meisam; Deshmukh, Abhijit V.; Sangid, Michael D. (Elsevier Ltd., 2017)
      Physics-based machining models typically require significant computational resources and time which makes them impractical for quick process optimization calculations in an industrial shop-floor setting. In this paper, we ...
    • Integration of airfoil stall and compressibility models into a propeller blade element model 

      Dorfling, Johann; Rokhsaz, Kamran (American Society of Civil Engineers, 2016-07)
      The blade element method is an indispensible engineering design tool. It executes rapidly on a personal computer and is capable of accurate propeller performance predictions. An extensive literature survey reveals that for ...
    • Introductory comparison of agricultural and single-engine air tanker operational loads 

      Rokhsaz, Kamran; Kliment, Linda K. (American Institute of Aeronautics and Astronautics, Inc., 2018-01-07)
      Flight loads of aircraft flown for agricultural applications have been compared with those flown as single-engine air tankers to assess the dependence of the load factors exerted on these airframes on the type of operation. ...
    • Kalman-Filter-Based Adaptive Control: flight testing on general aviation aircraft 

      Rafi, Melvin; Steck, James E.; Watkins, John Michael (American Institute of Aeronautics and Astronautics, Inc., 2017-09)
      Sensor noise and turbulence effects have been prevalent issues in control system design. Although a control system may respond well to “clean” input signals and commands in simulation, this may not be the case when a ...
    • Kinematics analysis of the chipping process using the circular diamond saw blade 

      Jerro, H.D.; Pang, Su-Seng; Yang, Chihdar Charles; Mirshams, R.A. (American Society of Mechanical Engineers (ASME), 1999-05)
      One of the primary goals in the design of a diamond blade cutting system is to reduce the cutting force. By understanding the fundamentals of the kinematics of the sawing operation, these forces can be lowered and even ...
    • Learning quantum annealing 

      Behrman, Elizabeth C.; Steck, James E.; Moustafa, Mohamed A. (Rinton Press, Inc., 2017-05-01)
      We propose and develop a new procedure, whereby a quantum system can learn to anneal to a desired ground state. We demonstrate successful learning to produce an entangled state for a two-qubit system, then demonstrate ...
    • Life of composites under variable-amplitude fatigue using ST method 

      Seneviratne, Waruna P.; Tomblin, John S. (American Institute of Aeronautics and Astronautics Inc, AIAA, 2021-01)
      The primary goal in a damage-tolerance certification program is to avoid catastrophic failure due to fatigue, corrosion, or accidental damage throughout the operational life of the aircraft. The damage-tolerance philosophy ...
    • Local bending containment in sandwich panels with sub-surface core damage 

      Keshavanarayana, Suresh R.; Ghimire, Ritesh (Sage, 2008-05-02)
      A simple repair technique to contain the local facesheet bending in sandwich panels with sub-surface core damage has been explored using experiments. The strategic filling of honeycomb cells in the damage region using ...
    • Low thrust orbit-raising using non-singular orbital elements and proximity quotient approach 

      Vijayan, Sainath; Dutta, Atri (Univelt, Inc., 2015)
      Recent years have shown a growing interest in the space industry in all-electric satellites. Mission designers analyzing the optimal deployment options for all electric satellites need to consider three important metrics: ...
    • Low-frequency noise control using layered granular aerogel and limp porous media 

      Xue, Yutong; Dasyam, Amrutha; Bolton, J. Stuart; Sharma, Bhisham N. (Institute of Noise Control Engineering, 2021-08-01)
      The acoustic absorption of granular aerogel layers with a granule sizes in the range of 2 to 40 μm is dominated by narrow-banded, high absorption regions in the low-frequency range and by reduced absorption values at higher ...
    • Low-thrust orbit-raising trajectories considering eclipse constraints 

      Sreesawet, Suwat; Dutta, Atri (Univelt, Inc., 2015)
      Many-revolution electric orbit-raising trajectories make numerous passages through the shadow of the Earth. The paper presents a new algorithm to determine the minimum-time trajectory of the spacecraft during orbit-raising. ...
    • Low-velocity impact and damage process of composite laminates 

      Guan, Zhidong; Yang, Chihdar Charles (SAGE Publications, 2002-04)
      Several important issues regarding damage simulation of composite laminates due to low velocity impact were investigated including contact law, damage initiation and the corresponding change of stiffness, and damping. ...
    • Machine learning applied to programming quantum computers 

      Steck, James E.; Behrman, Elizabeth C.; Thompson, Nathan L. (American Institute of Aeronautics and Astronautics, 2019-01-06)
      We apply machine learning to “program” quantum computers, both in simulation and in experimental hardware. A major difficulty in quantum computing is developing effective algorithms that can be programmed on a quantum ...
    • Minimizing errors from linear and nonlinear weights of WENO scheme for broadband applications with shock waves 

      Arshed, Ghulam Murshed; Hoffmann, Klaus A. (Elsevier, 2013-03-29)
      Improvements in the numerical algorithm for the dynamics of flows that involve discontinuities and broadband fluctuations simultaneously are proposed. These two flow features suggest numerical strategies of a paradoxical ...
    • Minimizing proton displacement damage dose during electric orbit raising of satellites 

      Dutta, Atri; Kasdin, N. Jeremy; Choueiri, Edgar Y.; Francken, Philippe (American Institute of Aeronautics and Astronautics, 2016-04)
      Although electric propulsion systems have been used in deep space missions for performing interplanetary transfers, their use has primarily been restricted to station-keeping purposes for Earth-orbiting satellites. ...
    • Minimum-fuel electric orbit-raising of telecommunication satellites subject to time and radiation damage constraints 

      Dutta, Atri; Libraro, Paola; Kasdin, N. Jeremy; Choueiri, Edgar Y.; Francken, Philippe (IEEE, 2014-06-04)
      The capability of a Geostationary satellite to perform electric orbit-raising enables the development of all-electric satellites. Key challenges to the realization of electric deployment of satellites to the Geostationary ...