NASA NACA-TR-1049-1951 Experimental investigation of the effect of vertical-tail size and length and of fuselage shape and length on the static lateral stability characteristics ofil s.pdf

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1、REPORT 1049.EXPERIMENTAL INVESTIGATION OF THE EFFECT OF VERTICAL-TAIL SIZE AND LENGTHAND OF FUSELAGE SHAPE AND LENGTH ON THE STATIC IKrERAL STABILITYCHARACTERISTICS OF A MODEL WITH 45 SWEFTBACK WINGAND TAIL SURFACES 1 -By M. J. QUEIJO “and WALTEB D. iioLHAESUMMARYAn. investigation was made to determ

2、ine the effects of certical-tail size and length and of fuselage shape and length on thestatic la%ral stability characteristics of a model u- ) t, r) * T0 = / ., -4-.002 / A +-j - AP A.:- .-.004. .-.-.002A-U.“Provided by IHSNot for ResaleNo reproduction or networking permitted without license from I

3、HS-,-,-1128 REPORT 104+NATIONAL ADIC(SORY COMMITITIE “FOR AERONAUTICSI I I I W+ F,V,I I I.-1 I , I I I .10.075.-t-.f50.225_:IA1 ,I I 1 I.(702-.-0 1 I I I I I I I I I I I I4 8 12 f6 20”24Angle of oftock,a, de.FIGL_RE2aTV+FI+V1Ti+Fi+T-It9b)IV+I%+V1 9 )-.,=+7. .81vd/T31meIege 8.0.026.OK1.076.100.125.15

4、0.200.260.W.a5.40.46.LK1.55.eo.66.TJ:il.s5.90.9sI.lmo.010$%.OaT.045.062.0s5.076.0a6.Om:g.100.0s9:!$!.Oaa.0T6.005:%?.02000.007.014.021.027.im.C09.049.067.066.02s.0T2.074.0T5.074.0i2SW.Cw.057.048.024.027.01400.005.010.014.ms.022.026.082.068.042.046.04s.049.050.049.0t8.IM6.M2.m.082.026.018.01000m.045.0

5、s.060.066.060.oi4.073.075.075:K.076.m4.072.068.Om.oEr.048.029.027.01$00.i.014.021.027.02a.02.9.04s.057:%.Oiz.074.Ois.075-075-on.Ooa.W6.2%?-cm.061:E-44TI”-I-FSn-+Fa+T”1TF+F1+Ii 9(C)TP-+R+T-aTF+F4IV+FL+TI lo(b).-J- -,-. . -.TF+FsIV+F+TZ H(b)IT+FY!-li *T7=+Fz+VJ- r-_-.-. 6,7,14#s&Fz 1$IVs+Fr!-H 14.Xotat!on (far &tei& em tebfe IU end 6&2t04):W wfn with aahwcfpt S, wfng wfthF tnrdegev vertlmf tan .82136374378Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-

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