Boundary-layer interaction effects in intakes with particular reference to those designed for dual subsonic and supersonic performance
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Word Count
5,500 words, Guess
Page Count
22 pages
Identifiers
- Library of Congress Control Number79499806
- Open LibraryOL4058493M
Classifications
- DDC629.13/008 s
- LCCTL526.G7 A4 no. 3565
Series Statement
- Aeronautical Research Council. Reports and memoranda, no. 3565
- Reports and memoranda (Aeronautical Research Council (Great Britain)) ;
- no. 3565.
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