Research on rotating stall in axial flow compressors. Part II. On the separation of the unsteady laminar boundary layer
By: R. A. Hartunian and F. K. Moore.
Contributors: Moore, F. K.; Wright Air Development Center
Series: WADC technical report -- 59-75
Publisher: Wright Air Development Center
Published: 1959
Place of publication: Wright-Patterson Air Force Base, Ohio
Number of pages: 25
Notes: Aeronautical Research Laboratory, Contract no. AF33(616)-3558, Project no. 3066, Task no. 70181.

Bibliographical references: p.20.

Contract number: AF-33(616)-3558