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  • FLUID MECHANICS  (2)
  • Structure, structural phase transitions, mechanical properties, defects  (1)
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  • 1
    facet.materialart.
    Unknown
    Structural distortions at polar manganite interfaces (2017)
    American Physical Society (APS)
    Details
    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
    Published by American Physical Society (APS)
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    PAPER CURRENT
  • 2
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    Separated flow over bodies of revolution using an unsteady discrete-vorticity cross wake. Part 1: Theory and application (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A method is developed to determine the flow field 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-flow fields which made up the entire flow field 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 aerodynamic bodies at low speeds and 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. In addition, three dimensional steady separation regions and wake vortex patterns are determined.
    Keywords: FLUID MECHANICS
    Type: NASA-CR-2414
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 3
    facet.materialart.
    Unknown
    Separated flow over bodies of revolution using an unsteady discrete-vorticity cross wake. Part 2: Computer program description (1974)
    In:  CASI
    Details
    Publication Date: 2019-06-27
    Description: A method is developed to determine the flow field of a body of revolution in separated flow. The computer was used to integrate various solutions and solution properties of the sub-flow fields which made up the entire flow field 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 two-dimensional unsteady separated flow problem based upon an unsteady, discrete-vorticity wake. Data for the forces and moments on aerodynamic bodies at low speeds and 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. In addition, three dimensional steady separated regions and wake vortex patterns are determined. The computer program developed to perform the numerical calculations is described.
    Keywords: FLUID MECHANICS
    Type: NASA-CR-2415
    Format: application/pdf
    Location Call Number Expected Availability
    BibTip Others were also interested in ...
    NASA TECHNICAL REPORTS
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