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  • AERODYNAMICS  (2)
  • Aerodynamics  (1)
  • Structure, structural phase transitions, mechanical properties, defects  (1)
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  • 1
    Publication Date: 2017-08-01
    Description: Author(s): S. Koohfar, A. S. Disa, M. S. J. Marshall, F. J. Walker, C. H. Ahn, and D. P. Kumah Electronic, lattice, and spin interactions at the interfaces between crystalline complex transition-metal oxides can give rise to a wide range of functional electronic and magnetic phenomena not found in bulk. At heterointerfaces, these interactions may be enhanced by combining oxides where the pola... [Phys. Rev. B 96, 024108] Published Mon Jul 31, 2017
    Keywords: Structure, structural phase transitions, mechanical properties, defects
    Print ISSN: 1098-0121
    Electronic ISSN: 1095-3795
    Topics: Physics
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  • 2
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    In:  Other Sources
    Publication Date: 2019-06-27
    Description: A method is developed to determine the flowfield of a body of revolution in separated flow. The technique employed is the use of the computer to integrate various solutions and solution properties of the sub-flowfields which make up the entire flowfield without resorting to a finite difference solution to the complete Navier-Stokes equations. The technique entails the use of the unsteady cross flow analogy and a new solution to the required two-dimensional unsteady separated flow problem based upon an unsteady discrete-vorticity wake. Data for the forces and moments on bodies of revolution at high angle of attack (outside the range of linear inviscid theories) such that the flow is substantially separated are produced which compare well with experimental data at low speeds. In addition, three-dimensional steady separation regions and wake vortex patterns are determined.
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft; 12; Feb. 197
    Format: text
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  • 3
    Publication Date: 2019-06-27
    Keywords: AERODYNAMICS
    Type: Journal of Aircraft; 12; Feb. 197
    Format: text
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  • 4
    Publication Date: 2019-06-27
    Description: A method is developed to determine the time-dependent flowfield about an impulsively started circular cylinder. An outer potential flow model is interfaced with an inner viscous flow region. The wake is described by a set of elementary point vortices. The position at which the point vortices are shed from the cylinder is obtained from a solution to the unsteady incompressible laminar boundary-layer equations. A rear shear-layer is postulated to account for backflow induced vorticity. Wake development is detailed from the initial formation of the two symmetric vortices to subsequent asymmetry and eventual alternate shedding. Unsteady pressure distributions, lift and drag forces, and Strouhal number are calculated and compared with experiment.
    Keywords: Aerodynamics
    Type: AIAA Journal; 14; July 197
    Format: text
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