Pressure distributions on planar and cruciform delta wings attached to cylindrical bodies in supersonic flow
part 1-theoretical results for the wing thickness case
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Author
Contributions
- Sheppard, L. M., joint author. - Contributor
Publication
1966 - Dept. of Supply, Australian Aeronautical Research Committee, Melbourne, Australia
Language
English
Word Count
20,500 words, Guess
Page Count
82 pages
Identifiers
- Library of Congress Control Number73490390
- Open LibraryOL5516356M
Classifications
- LCCTL507 .A8 no. 69
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