NASA NACA-TN-3797-1956 Section characteristics of the NACA 0006 airfoil with leading-edge and trailing-edge flaps《带有前缘和后缘襟翼的NACA 0006机翼的截面特性》.pdf

1、I.;.iNATIONALADVISORYCOMMITTEEFOR AERONAUTICSTECHNICAL NOTE 3797SECTION CHARACTERISTICS OF THE NACA 0006 AIRFOILWITH LEADING-EDGE AND TRAILING-EDGE FLAPSBy Bruno J. GambucciAmes Aeronautical LaboratoryMoffett Field, Calif.WashingtonDecember 1956;l-, 1,.,J: 35, ad 500, 35, and 500, 35, and 500, 35, d

2、 50102025303540503(b)3(c)3(d)3(e)j(f)3(8)3(h)-II(f) to II(h)-II(i) to II(k)-TABLE II.- PRESSURE DISTRIBUTIONFOR THE NACA 0006AO(a) bn = OO; bf = 0Angleofat-tadsa. d a.4J.#Ia -6.28 0a -8.30 I a - 10.” a . 1.2.27“Ichmauisestation(QercentEdrfoflchord)m.6s.23.07-.*-.13-J.-.J-.14-.14-.lk-.13-.X2-m.-.10-.

3、*-.08-.o-.06-.04-.03-.02-.01Lauer Jpper Luwer=3-1.53-1.37-1.37-1.37-1.38-1.38-1.36-1.35-1.16:g-.66x-.40-.34-.29-25-.16-.14-.I.2-.10m-1.*-1.26-1 .a.-1 J2-1.02-1.00-1.00-3. .m-1.m-.93“.*-.97x-.s-.ea-.84-.-.E-.57-.9-.5344 :io o.%-2A. .g5-1.“3.93 . bf = 20a . 1.290I a . 2.230a-e. O$ :?;z;g -1.ki-k .3 -.

4、?3-.-.79 ; :3-fi -.80-.73 z -77-.n -.PJ :Z:; g :$-1.11 -A-1.26 -1.22-1.1o +.42:$ z -:;g:44 -Al-.37-.39 .09 -.=3 G-1.W-1.6s-l.%-1.fi?-1.53-l.%-1.%-l.%-l.%-1.3i?-1.52.3?-1.2:%-.55-.05-.0):g-.-.73-.63-.64-Al-.x-.% 0.560.1.5 g-1.02.05.07-5 -.0510.0 -Jo - Lb20 -s-=39 -.9-.33G -.37 -Al -.4555 -.2a -.af-b

5、-.79-1 a -1.40 -1.*1* -;84.33 -.30J.2 :g93.so1.s1.02.0.o7-sI.o.o1.2.5-al$5i%45P535f = 35a . 4.3#a .1.24 I a-i?. 2!%a . -lo .aO G . -1.glo a . O.ufm=G+.(IJ+?.B-2*.l.p.1s.l.UI-.06-.77-.70-.68-.65-.65-.63-.-.63-.61.-.63-.72-.*.1.1o.1-25-.60-.57J-.53-.algi?45P55bf = 70a. -1.no a-2. #b“An of attack a . -

6、14J40 a-odzzE-2Se-2 .a2Q.CQ-2.2-2.03-2.W-2.08-2J.o-2.13-2.11.-2.05-1.%-1.%?-1.654.47-1.3-lJT-1 .Ca-1.034.0-d-1.01.-.9.-.Ea-.87-.89-.9over3cudvis(pm-centchcd:m=o.l1:2.05.07.5E:;aZJii?%O.*;.42.42.471 I10.27I .10 -.62 -.62-.46-.20-z-Se-ml Jaif! .35:%7.2xl.3.0J_.W -=.Q7 -ar.x -.,1 -4255 I h I .04j .,.,!

7、(g) = 20; Sf 35FAngle of attackImmtuisemtatim a.ml=a-%=m-0p-4.18-3 Ap-2.f22-2J2-1 .n-1 .$X3-2U-5.CQ-3 .%-3.25Q.75-1.sg-1.53-1.33-1.lg-1.03-l.-.96-.9-.88-.86-.95-1.03-;g64-.64-.65-.65-dmrd)09P=IrfwlLunrG:3J.53Jo-.x?-.33-.%+2.3:3-1 J.4-.77:2-5)-99-.73-.-.6?-.63-.P-.9-1.J74.9-.62-.$ -3 :Ca.n -2.W -1.65

8、.63 -1.43 -1.27.64 -ld5 -1.07; :g -.W -.95 :gx -.6?-.; -.62.38 -.62.28 -.6?o8lo-1.%-1.31-1 ml-.73.65%.W.2.25.48.921.m:%. bf = W“Angle of attack e. . Ody I a-z. 2$ F-a - 6.U0a . -3. S a.m=TG-6.67:E-2.77-2 J6-2.03-2.ca-2.28:-3m-2.EJ-2.fx-1.62-1.42-1.2g-1.21-1 J4-1 m-1.09-1.06-1 .W-1.39-1.46-1.47- .*-.

9、W-.9-.9- .P*k-wakmdHiOc Htdx.Onpementairfoil.%ud) JPma23.3s.1.2-.22-.42-.6?-.0.3.aJ.2.15.l.n.1.X.1.04:%-.:%I.o.a-aw40z6573.2J13mm.z05.990.Cg-.23lb-.03.la.400.134.23-1.2 :;:g.83 -1.1o- -1.42 -l.% -1.5-.%z -.5Q-.%z - .5Q.43 - .%.* - .%0.531.W.97g.68.72cl.1.(XI.%.9J.72 -75.49 .65 -n.53 .64.83 .8s.77.%-

10、*.lSA?.44.25.a5.47.=(i) bn = 30; f = 0G -10.340mm -o. - J8 o .fl-.47 .65; g-1 .m .x-1 .2? .-.93 :E G-37 .22-.3-.15 -u 2-07 - .a? .10+.4P a.1 .55”k-uel-0 .y3Jz1.m.95a).77.79x%T7z.34.9J.9.lf15An. of atbckXQr %-1.36-1J.4-.98:%-.29-.25-.23- J.9-.1?-.l-.13-J2- J.O-.07-.W-.03-.02-?-.47-.46:%- m=G. bf = 35

11、TFa.k J-3.P-g :$ -1-io . -1.a5.76 - m z - .*l-nY5:%z-1.ls I l-g.07 33LZ1 AndaarattsekmI-7121- 0.841.CU:ij.7?-3.-e Al -am% -2.(- ;-m-1.3?-la: ;:$, ;-lJ6 4.24-la -1 .lJr -1 -w .Tf -1.1o-1 al .23 -1.&5 z-.B m -La? A%-1,1 -1.3-.-.-.%-.6)-.03-1.2:.Jg-&-.& -.%?-.%? S2.84x.24 - 1Provided by IHSNot for Resa

12、leNo reproduction or networking permitted without license from IHS-,-,-NACA TN 3797Figure.A-1911661.-The NAcA 0006 airfoil mounted in the Ames 7- by 1tunnel. ,“.O-footIllwind. - . -. .Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-Stulkm,pacmi cT 0

13、/( ,0 I 5,0 070.0 0100cf -k, c4.w$*+Ifhqe H 1,/W (max. MkoilmJFigure 2.- Geometm of the UK&J. .Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-NACA TN 3797 132401.61.2.8%.40-.4-.8c1-16 -8 0 8 16 0 -.1 -.2 -.3 -.4a, deg cm(a) 8n=002.01.6I .2.8.40-.4-.

14、8 -16 -8 0 8 16 0 -. I -.2 -.3 -.4a, deg cm(b) 8n=100Figure 3.- Section lift and pitching-momentcharacteristics. . . . . .Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-14 IwcA TN 3797c1c,mL6E.8.40-.4-1q deg %-l(c) 8n=20”201.612.840-4-16 -8 0 8 16 0

15、 -J -.2 -.3 -4a, deg %(d) Zln=250.Figure 3.- Continued.Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-152.01.61.2.8.40-.4 -8 0 8 16 .1 0 . I -.2 .3 .4a,deg cm(e)8n=302.01.6I .2%.8.40-.4 -8 0 8 16 .1 0 . I -.2 -.3 .4a, deg cm(f) an= 35Figure 3.- Cont

16、inued. .- _ . . . . . Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-16.1.2Ct.82.01.6.40a.,8 O 8 16 .1 0 .1 -.2 -.3 -4a, deg %1g) =40”2.01.61.2c1 .8.40A.T-8 0 8 16 J o -.1 .2 -.3 -.4a, deg %(h) =50*,.Figure 3.- Concluded.Provided by IHSNot for Resal

17、eNo reproduction or networking permitted without license from IHS-,-,-172.4201cl max1.2.8!4A L/ /( h/8f, dego 0A 20n 350 50v 70.00 10 20 30 40n,degFigure 4.- Variation of -mum lift with nose flap deflection.NACA -Langley Field, VA.50. . .Provided by IHSNot for ResaleNo reproduction or networking permitted without license from IHS-,-,-