NASA NACA-RM-A7H29-1948 High-speed aerodynamic characteristics of horn and overhang balances on a full-scale elevator《全比例电梯喇叭和突出部分平衡的高速空气动力特性》.pdf
《NASA NACA-RM-A7H29-1948 High-speed aerodynamic characteristics of horn and overhang balances on a full-scale elevator《全比例电梯喇叭和突出部分平衡的高速空气动力特性》.pdf》由会员分享,可在线阅读,更多相关《NASA NACA-RM-A7H29-1948 High-speed aerodynamic characteristics of horn and overhang balances on a full-scale elevator《全比例电梯喇叭和突出部分平衡的高速空气动力特性》.pdf(84页珍藏版)》请在麦多课文档分享上搜索。
1、RM NO. A7HZ9 - RESEARCH MEMORANDUM HIGH-SPEED AERODYNAMIC CHARACTERLSTICS OF HORB AND OVEREANG BALANCES ON A FULL-SCALE ELEVATOR BY Joseph W. Cleary and Walter J. Rrumm Ames Aeromuticrl Laboratory Moffett Field, Calif. 0 TECHNICAL EDITING WAIVED NATIONAL ADVISORY COMMITTEE FOR AERONAUTICS WASHINGTON
2、 N A C A LIBRARY Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-3 1176 01360 5267 “- .- * By Joseph W. Cleary and Walter J. Biwnm SUMMARY High-speed wind-tmnel tests have been conducted of horn- and overhang-kahme elemtors on a full-scale, semispan,
3、 horizontal tail. The effects of unshielding the horn and of unsealing the - L tc werhang were investigated. *K. t-7 .- . . A?-!? . i Analysis of the data shows that shielded-born bdances can be/. .*y- “. used advantageously to give 8 positive rate of change of hinge- mcment coefficient with angle o
4、f attack, or when used in conjufction with an mer- balaace to limit this quantity to a small value. Although mahielding the horn caused considerable overlalancing and a relatively large positive rate of change of hiwcmnt coeffi- cient with angle of attack, these quantities can be regulated by approp
5、riately chooslng the horn area and. chord, Cowre- cawed slight merb b-es with shielded and unshielded tip. Parameters Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-6 EAGA RM No. Am expressing the variation of the lift-curve slope C parmters produce
6、d a - u T,Y- rruarerical decrein me fkcm -0.50 to -0.283” the same FB shown in figure 35 for 0 -e of attack and several elevatm asgles. Since the critical ro I 1.490 I 1.696 2.850 b690 1.424 1.636 1.184 1.712 1.083 1.443 + 1.815 8.05 I 1.815 8.420 1.748 9.669 1.630 o Stmight lines from station 4.532
7、 inelids to trolllng edge mdius. 6 Stralght lines from statlm 3662 inclHs to troilfng edge radius. .( . . Z ? Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-. . . . . . . . - - rr . # k TABLE llIrSUMMARY OF THE ELEKAm CHLIRACERISTICS L 4 Noie - Valu
8、es of parameters are for tmd 6, of O? Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Fig. 1 NACA RM No. A7HZ9 . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA RM No. A7H29 (a) Front view. . . #
9、 Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA RM No. A7H29 Fig. 3 Shielded normol-nose horn balance Unshieldad normal-nose horn balance NATlOflAL ADVISORY COWLUTTLL FOR AERONAUTICS Unshielded eilitical-nose horn balance -/oas “-4 -crL Overhan
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