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Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber
Author(s): Hartunian, R. A.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report number: WADC TR 59-75 Part 1
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Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer
Author(s): Hartunian, R. A., Moore, F. K.
Corporate Author(s): Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Report number: WADC TR 59-75 Part 2

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