Influence of cut-outs in elevator on static longitudinal stability and on static elevator effect; in order to improve rudder effect of sport airplane at high angles of attack, cut-out was made in center of continuous elevator so as to enlarge rudder downward; static controllability resulting from cut-out manifested 18% drop in elevator effect at full throttle and 10 to 20% drop at idling. (see also Nat Advisory Committee Aeronautics -- Tech Memo n 750 Aug 1934 4 p 3 supp plates)
Influence of cut-outs in elevator on static longitudinal stability and on static elevator effect
Einfluss eines Ausschnittes im Hoehenruder auf die statische Laengsstabilitaet und die statische Hoehenruderwirkung
Luftfahrtforschung ; 11 , n 1
1934
4 pages
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Article (Journal)
German
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Influence of cut-outs in elevator on static longitudinal stability and on static elevator effect
Engineering Index Backfile | 1934
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