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Analysis of limitations imposed on one-spool turbojet-engine designs by compressors and turbines at flight Mach numbers of 0, 2.0, and 2.8
- Author / Creator
- Available as
- Online
Details
- Creator
- by Richard H. Cavicchi and Robert E. English
- Included Title
-
- Technical Report Archive & Image Library (TRAIL)
- Format
- Books
- Language
- English
- Contributors
- Publication
-
- Washington [D.C.] : National Advisory Committee for Aeronautics, [1954]
- Physical Details
-
- 1 online resource (50 pages) : illustrations
- data file
- OCLC
- ocn885060404
- Cover title.
- On front cover: "September 24, 1954."
- Includes bibliographical references (page 33).