NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Collections About News Help Login
Back to Results
Application of Supersonic Vortex-flow Theory to the Design of Supersonic Impulse Compressor- or Turbine-blade Sections
Document ID
19930087012
Acquisition Source
Legacy CDMS
Document Type
Other
Authors
Wlodarski, John
Sterrett, James R
Boxer, Emanuel
Date Acquired
August 16, 2013
Publication Date
April 24, 1952
Report/Patent Number
NACA-RM-L52B06
Report Number: NACA-RM-L52B06
Accession Number
93R16302
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.

Related Records

There are no records associated with this record.
No Preview Available