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  • AERODYNAMICS  (4)
  • 33-315A; Alteration; Caesium; Cerium; Chromium; Cobalt; Comment; Deep Sea Drilling Project; DEPTH, sediment/rock; DRILL; Drilling/drill rig; DSDP; DSDP/ODP/IODP sample designation; Europium; Gadolinium; Glomar Challenger; Hafnium; Leg33; Lithology/composition/facies; North Pacific/FAN; Rock type; Sample code/label; Sample ID; Sample method; Scandium; Tantalum; Terbium; Thorium; Uranium; Visual description; Ytterbium; Zinc; Zirconium  (1)
Collection
Keywords
Publisher
Years
  • 1
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    Unknown
    Minor-element chemical analyses of Hole 33-315A (2005)
    PANGAEA
    Details
    Publication Date: 2023-07-10
    Keywords: 33-315A; Alteration; Caesium; Cerium; Chromium; Cobalt; Comment; Deep Sea Drilling Project; DEPTH, sediment/rock; DRILL; Drilling/drill rig; DSDP; DSDP/ODP/IODP sample designation; Europium; Gadolinium; Glomar Challenger; Hafnium; Leg33; Lithology/composition/facies; North Pacific/FAN; Rock type; Sample code/label; Sample ID; Sample method; Scandium; Tantalum; Terbium; Thorium; Uranium; Visual description; Ytterbium; Zinc; Zirconium
    Type: Dataset
    Format: text/tab-separated-values, 192 data points
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    DATA PANGAEA
  • 2
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    On the analytic structure of the Taylor-Maccoll conical-flow solution (1975)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: The conical flow solution for axisymmetric supersonic flow past cones has been found to be virtually independent of the ratio of specific heats when normalized in a certain way. A simple rational approximation to this flow is derived. The important singularities and the limiting behavior of the solution are also discussed.
    Keywords: AERODYNAMICS
    Type: Zeitschrift fuer angewandte Mathematik und Physik; 26; July 25
    Format: text
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    NASA TECHNICAL REPORTS
  • 3
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    Series solution for the planar asymmetric blunt-body problem (1975)
    In:  Other Sources
    Details
    Publication Date: 2011-08-16
    Description: Accurate semianalytic solutions to the inverse blunt-body problem have been obtained using a method of series expansion. Rational fractions are employed for series summation and analytic continuation. Angles of incidence up to 30 deg and Mach numbers as low as 2 have been considered. The maximum-entropy streamline will not wet the body surface in asymmetric flow. It may pass either above or below the stagnation streamline. Limit lines appear in the supersonic portion of the flow field, both in the shock layer and in its upstream analytic continuation.
    Keywords: AERODYNAMICS
    Type: Physics of Fluids; 18; Dec. 197
    Format: text
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    NASA TECHNICAL REPORTS
  • 4
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    A semi-analytic approach to the self induced motion of vortex sheets (1980)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: The rolling up of the trailing vortex sheet produced by a wing of finite span was calculated as a series expansion in time. For a vorticity distribution corresponding to a wing with cusped tips, the shape of the sheet was found by summing the series using Pade approximants. The sheet remains analytic for some time but ultimately develops an exponential spiral at the tips. The centroid of vorticity was conserved to high accuracy.
    Keywords: AERODYNAMICS
    Type: NASA-CR-166182 , SU-JIAA-TR-32
    Format: application/pdf
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    NASA TECHNICAL REPORTS
  • 5
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    A semi-analytic approach to the self-induced motion of vortex sheets (1981)
    In:  Other Sources
    Details
    Publication Date: 2019-06-28
    Description: The rolling-up of the trailing vortex sheet produced by a wing of finite span is calculated as a series expansion in time. For a vorticity distribution corresponding to a wing with cusped tips, the shape of the sheet is found by summing the series using Pade approximants. The sheet remains analytic for some time but ultimately develops an exponential spiral at the tips. The centroid of vorticity is conserved to high accuracy.
    Keywords: AERODYNAMICS
    Type: Journal of Fluid Mechanics; 111; Oct. 198
    Format: text
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    NASA TECHNICAL REPORTS
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