Reasons for low aerodynamic performance of 13.5-centimeter-tip-diameter aircraft engine starter turbine
By: Jeffrey E. Haas, Richard J. Roelke, Paul Hermann
Contributors: Roelke, Richard J; Hermann, Paul; United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch; Propulsion Laboratory (U.S.)
Series: NASA technical paper -- 1810; AVRADCOM technical report -- 80-C-17
Publisher: National Aeronautics and Space Administration, Scientific and Technical Branch; For sale by the National Technical Information Service]
Published: 1981
Place of publication: Washington, D.C; [Springfield, Va
Language: eng
Number of pages: 16
Subjects: Airplanes -- Motors -- Evaluation
Notes: "Propulsion Laboratory, AVRADCOM Research and Technology Laboratories, Lewis Research Center."

"March 1981"--Cover