Aerodynamic effect of a honeycomb rotor tip shroud on a 50.8-centimeter-tip-diameter core turbine
By: Thomas P. Moffitt and Warren J. Whitney
Contributors: Whitney, Warren J; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Series: NASA technical paper -- 2112
Publisher: National Aeronautics and Space Administration, Scientific and Technical Information Branch; For sale by the National Technical Information Service]
Published: 1983
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 16
Subjects: Turbomachines
Notes: "January 1983"--Cover

STAR category 07

Includes bibliographical references