columbus · Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber

Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber

Title: Research On Rotating Stall In Axial Flow Compressors. Part I: On Lift Hysteresis At Maximum Lift Including Effect Of Camber
Date: 1959
Index Abstract: Limited
Photo Quality: Not Needed
Report Number: WADC TR 59-75 Part 1
Creator: Hartunian, R. A.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Extent: 34
PB Number: PB151948
Identifier: AD0216301
Access Rights: OTS
Distribution Classification: 2
Contract: AF 33(616)-3558
DoD Project: 3066
DoD Task: 70181
DTIC Record Exists: No
Distribution Change Authority Correspondence: None
Distribution Conflict: Yes
Report Availability: Not available via Contrails
Date Issued: 1959-01
Abstract: The abstract for this report is either unavailable or has yet to be entered
Provenance: Bearcat
Type: report