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    A review of some Reynolds number effects related to bodies at high angles of attack (1984)
    In:  CASI
    Details
    Publication Date: 2019-06-28
    Description: A review of some effects of Reynolds number on selected aerodynamic characteristics of two- and three-dimensional bodies of various cross sections in relation to fuselages at high angles of attack at subsonic and transonic speeds is presented. Emphasis is placed on the Reynolds number ranges above the subcritical and angles of attack where lee side vortex flow or unsteady wake type flows predominate. Lists of references, arranged in subject categories, are presented with emphasis on those which include data over a reasonable Reynolds number range. Selected Reynolds number data representative of various aerodynamic flows around bodies are presented and analyzed and some effects of these flows on fuselage aerodynamic parameters are discussed.
    Keywords: AERODYNAMICS
    Type: NASA-CR-3809 , NAS 1.26:3809
    Format: application/pdf
    Location Call Number Expected Availability
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