Showing 1 - 9 results of 9 for search 'Brown, Clinton E', query time: 0.70s Refine Results
  1. 1
    Theoretical lift and drag of thin triangular wings at supersonic speeds /
    by Brown, Clinton E
    Published 1946

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  2. 2
    Damping in pitch and roll of triangular wings at supersonic speeds /
    by Brown, Clinton E
    Published 1948

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  3. 3
    Theoretical lift and drag of thin triangular wings at supersonic speeds /
    by Brown, Clinton E
    Published 1946

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  4. 4
    The reversibility theorem for thin airfoils in subsonic and supersonic flow /
    by Brown, Clinton E
    Published 1949

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  5. 5
    On slender delta wings with leading-edge separation /
    by Brown, Clinton E
    Published 1955

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  6. 6
    Investigation of minimum drag and maximum lift-drag ratios of several wing-body combinations including a cambered triangular wing at low Reynolds numbers and at supersonic speeds /
    by Brown, Clinton E
    Published 1958

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  7. 7
    Preliminary wind-tunnel tests of triangular and rectangular wings in steady roll at Mach numbers of 1.62 and 1.92 /
    by Brown, Clinton E
    Published 1956

    This item is not available through BorrowDirect. Please contact your institution’s interlibrary loan office for further assistance.
    Government Document Book
  8. 8
    An analysis of performance estimation methods for aircraft /
    by Brown, Clinton E
    Published 1967

    Book
  9. 9
    Evaluation of effectiveness of various devices for attenuation of trailing vortices based on model tests in a large towing basin /
    by Kirkman, Karl L
    Published 1973
    Other Authors: “...Brown, Clinton E...”

    Book
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