Measurement results for Russian laminar profile 2315 Bis with nose flap are given where form, magnitude, and angle of attack of flap had been changed systematically. English translation from ZWB Forschungsbericht n 1948 June 13 1944.
Systematic wind-tunnel measurements on laminar wing with nose flap
Nat Advisory Committee Aeronautics -- Tech Memo
1947
7 pages
10 Supp Plates
Report
English
© Metadata Copyright Elsevier B. V. All rights reserved.
Wind Tunnel Testing of a Blown Flap Wing
AIAA | 2019
|Engineering Index Backfile | 1947
|DataCite | 2021
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