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Report No. 614, Pressure distribution over an N.A.C.A. 23012 airfoil with an N.A.C.A. 23012 external-airfoil flap: By Carl J. Wenzinger. 15 pages, illustrations, 23 × 29 cms. Washington, Government Printing Office, 1938. Price 10 cents

Publisher: Elsevier Science
Year: 1938
Tongue: English
Weight: 125 KB
Volume: 225
Category: Article
ISSN: 0016-0032
DOI: 10.1016/s0016-0032(38)90723-9

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