Effect of stator blade orientation on the performance of an axial flow compressor
Contributors: Naval Postgraduate School (U.S.)
Publisher: Naval Postgraduate School
Published: 1967
Place of publication: Monterey, California
Language: eng
Subjects: Aeronautics
Notes: Thesis (Aeronautical Engineer)--Naval Postgraduate School, 1967.

Bibliography: p. 111-112.

Approved for public release, distribution unlimited.