Investigation of Rotating Stall in a Single-Stage Axial Compressor Page: 4 of 29
This report is part of the collection entitled: National Advisory Committee for Aeronautics Collection and was provided to Digital Library by the UNT Libraries Government Documents Department.
The following text was automatically extracted from the image on this page using optical character recognition software:
NACA TN 3823 3
p separation between inlet guide vanes and rotor
Ps static pressure
rt rotor tip radius
U rotor velocity at mean radius
V stall-propagat ion velocity at mean radius relative to rotor
w inlet velocity relative to rotor
x,y coordinate directions
al absolute air angle entering rotor
m2 absolute air angle leaving rotor
P1 air inlet angle relative to rotor
P2 air outlet angle relative to rotor
perturbation velocity potential
angular frequency of stall propagation
Here’s what’s next.
This report can be searched. Note: Results may vary based on the legibility of text within the document.
Tools / Downloads
Get a copy of this page or view the extracted text.
Citing and Sharing
Basic information for referencing this web page. We also provide extended guidance on usage rights, references, copying or embedding.
Reference the current page of this Report.
Montgomery, S. R. & Braun, J. J. Investigation of Rotating Stall in a Single-Stage Axial Compressor, report, January 1957; (digital.library.unt.edu/ark:/67531/metadc56040/m1/4/: accessed October 20, 2018), University of North Texas Libraries, Digital Library, digital.library.unt.edu; crediting UNT Libraries Government Documents Department.