National advisory committee for aeronaut
📂
Article
📅
1937
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Elsevier Science
🌐
English
⚖ 68 KB
BOOK REWEWS. 401 thickness. Structural and stability problems associated with the large negative pitching moments occurring at high-lift coefficients may be slightly greater than in the case of ordinary and split flaps. Report No. 574. Pressure Distribution Over an Airfoil Section with a Flap and