An approximate method for determining the incompressible, irrotational flow around a symmetrical wing section
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Author
Publication
1949 - Division of Aeronautics, Royal Institute of Technology, Stockholm, Sweden
Language
English
Word Count
0 words, Guess
Page Count
0 pages
Identifiers
- OCLC Control Number10945413
- Open LibraryOL54253859M
Subjects
Series Statement
- K[ungl.] T[ekniska] H[ögskolan] AERO T[echnical] N[ote] -- no. 7
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