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  • Other Sources  (3)
  • NASA Technical Reports  (3)
  • Aerodynamics  (3)
  • AERODYNAMICS
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  • Spacecraft Design, Testing and Performance
  • 2005-2009
  • 1955-1959
  • 1950-1954
  • 1930-1934  (1)
  • 1925-1929  (2)
  • 1933  (1)
  • 1925  (2)
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  • Other Sources  (3)
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  • NASA Technical Reports  (3)
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  • 2005-2009
  • 1955-1959
  • 1950-1954
  • 1930-1934  (1)
  • 1925-1929  (2)
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  • 1
    Publication Date: 2019-06-28
    Description: This report contains those results of the theory of wings and of wing sections which are of immediate practical value. They are proved and demonstrated by the use of the simple conceptions of "kinetic energy" and "momentum" only, familiar to every engineer; and not by introducing "isogonal transformations" and "vortices," which latter mathematical methods are not essential to the theory and better are used only in papers intended for mathematicians and special experts.
    Keywords: Aerodynamics
    Type: NACA-TR-191
    Format: application/pdf
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  • 2
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    In:  CASI
    Publication Date: 2019-06-28
    Description: Progressive application of the Kutta-Joukowsky theorem to the relationship between airfoil lift and circulation affords a number of formulas concerning the conduct of vortex systems. The application of this line of reasoning to several problems of airfoil theory yields an insight into many hitherto little observed relations. This report is confined to plane flow, hence all vortex filaments are straight and mutually parallel (perpendicular to the plane of flow).
    Keywords: Aerodynamics
    Type: NACA-TM-713
    Format: application/pdf
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  • 3
    Publication Date: 2019-06-28
    Description: In the first article, in connection with a lecture on the hydrodynamic basis of flight and the potential flow about a Joukowski wing, the pressure distribution on several wings is computed and plotted. The diagrams of the pressure distributions are presented accompanied with a qualitative discussion of the pressure distribution. In the second article, the the cross-sectional outline (or profile) a Joukowski wing are plotted.
    Keywords: Aerodynamics
    Type: NACA-TM-336
    Format: application/pdf
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