http://www.loc.gov/mods/v3 http://www.loc.gov/standards/mods/v3/mods-3-2.xsd
design and testing of an axial-flow compressor having different blade profiles in each stage
Aeronautical Research Council (Great Britain)
"N.G.T.E. Report R.217, received March, 1958" -- page [1].
Includes bibliographical references (page 10).
Reports and memoranda (Aeronautical Research Council (Great Britain)) ; no. 3183