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Performance of an axial-flow compressor-rotor designed for a pitch-section lift coefficient of 1.20
- Author / Creator
- Available as
- Online
Details
- Creator
- by L. Joseph Herrig and Seymour M. Bogdonoff
- Included Title
-
- Technical Report Archive & Image Library (TRAIL)
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington, D.C. : National Advisory Committee for Aeronautics, 1947
- Physical Details
-
- 1 online resource (8, [10] pages) : illustrations
- data file
- OCLC
- on1231501103
- "Langley Memorial Aeronautical Laboratory."
- Title from title screen (viewed January 11, 2021)
- Date of issue: July 1947.
- Report numbers NACA-TN-1388.
- Includes bibliographical references (page 7)
- Electronic reproduction. Denton, Texas : University of North Texas, 2011. Electronic reproduction from print master produced by University of North Texas.