An experimental investigation of the flow through inclined circular tubes at a mach number of 4.0
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Word Count
4,000 words, Guess
Page Count
16 pages
Identifiers
- Library of Congress Control Number67093691
- Open LibraryOL5579819M
Classifications
- DDC629.134/353
- LCCTL507 .G77 no. 884
Subjects
Series Statement
- [Great Britain] Aeronautical Research Council. Current papers,
- no. 884
- Current papers (Aeronautical Research Council (Great Britain)) ;
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