Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer
Report Number: WADC TR 59-75 Part 2
Author: Hartunian, R. A.
Author: Moore, F. K.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Date of Publication: 1959-01
Pages: 33
Contract: AF 33(616)-3558
Project: 3066
Task: 70181
PB Number: PB161072
AD Number: AD0216302
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bearcat
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Via the Defense Technical Information Center (DTIC): This report is not publicly available via DTIC Via National Technical Information Service: This report is unlikely to be available in the National Technical Reports Library Indications of Public Availability A PB Number, PB161072 , exists for this report, indicating public availability of the report at time of publication No digital image of an index entry indicating public availability is currently available The inside cover of this report indicates that it was released for public saleRelated Reports
This report has the following parts/volumes:
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Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber
WADC TR 59-75 Part 1 -
Research On Rotating Stall In Axial Flow Compressors. Part III: Experiments On Laminar Seperation From A Moving wall
WADC TR 59-75 Part 3 -
Research On Rotating Stall In Axial Flow Compressors. Part IV: A Preliminary Study Of Three-dimensional Rotating Stall
WADC TR 59-75 Part 4