columbus · Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer

Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer

Title: Research On Rotating Stall In Axial Flow Compressors. Part II. On The Separation Of The Unsteady Laminar Boundary Layer
Date: 1959
Index Abstract: Limited
Photo Quality: Not Needed
Report Number: WADC TR 59-75 Part 2
Creator: Hartunian, R. A.; Moore, F. K.
Corporate Author: Cornell Aeronautical Laboratory, Inc.
Laboratory: Aeronautical Research Laboratory
Extent: 33
PB Number: PB161072
Identifier: AD0216302
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