1、f-tin/copy 208RML54H19. .,.RESEARCH MEMORANDUMAN INVESTIGATION OF A SUPERSONIC AIRCRAFT CONFIGURATIONHAVING A TAPERED WING WITH CIRCULAR-ARC SECTIONSAERODYNAMICAND 40 SWEEPBACKCHARACTERX3TICS OF THE CONFIGURATION EQUIPPEDWITH A CANARD CONTROL SURFACE AT A MACE NUMBERBy M. Leroy Spearmm and Edward B.
2、 PalazzoLangley AeronauticalLangley Field,LaboratoryVa.OF 1.89NATIONAL ADVISORY COMMITTEEFOR AERONAUTICSWASHINGTONOctober 18, 1954-,.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-.a71.icy . . . . . . . . . . . ; , ;,- /. ., -t . . .?.+., f,. : b.a,
3、.Ib . ./$=%+-=ww4bbbbbb.,., . . . .m .-f . . . . . . .RP.GE 0 OFf!CLk MAKING CHANGEJ,/.-,. ., J- / /,.= I 1111111 VIII Ideg ,+-1-dv,0 / 0 / -.51/ -.4?,-.3/ / / -.242 Y4 .5 .6 .7 .8 .9 Lo.a,decj.Cx.: ll.- Trim longitudinal characteristics. M = 1.89; it = -8.Provided by IHSNot for ResaleNo reproductio
4、n or networking permitted without license from IHS-,-,-NACA RJiL54H19 2102v=.1 10 Completemodel ,.c= 0“, iy-s:Y0TY= u = O“.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-22 NACA FM L54EL9Vx#iJtiL 1-.08j-.”w Ls4&Ai.+.-050 Complete model , & = 0“, I*-
5、 - 8“J V Camrd off,it=-8”L Vertical# horizontal tai I off, canard on ,Sc = 0G Vertical $ horizontal tai I offj cawd offv.+.-=5:-.1-4 0 4 8 12 16 20 24 28 32 36 40 44Angle of sideslip, deaa71Figure 12.- Concluded.NACA-Langley -10-18-54-950bProvided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-
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