Report deals with development of method which gives lucid and convenient solution of low conditions in vicinity of common, thick airfoil section wherein thickness of profile is taken into account. Bibliography. From Jahrbuch 1938 der Deutschen Luftfahrtforschung.
Two-dimensional potential flow past ordinary thick wing profile
Nat Advisory Committee Aeronautics -- Tech Memo
1942
51 pages
9 Supp sheets
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Subsonic gas flow past wing profile
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