NASA Technical Paper 2256 - CAFE Foundation

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TABLE 4.- Continued (b) VariEze winqlet root (x/c) U (z/c) U (x/c)L (z/c)L 0 00000 00250 00500 01060 015OO 02000 03000 04000 06000 08060 10000 12500. 15000 175O0 20000 ,22500 25000 27500 30000 32500 35000 37500 40000 42500- 45000 47500 50000 52500 55000 57500 GO000 62500 65000 .67560 70000 72500 75000 77500 80000 82560- 85000 87500 .90000 ,92500 ,95000 .97560 1.00000 0 00000 01150 01550 02150 02600 02900 03500 04000 04950 65706. 06500 07300 08050 08700 09250 69806 10300 10750 1.1150 11500 11700 11906 12000 12050 12000 11900 11700 11406 11000 10650 10200 09700 09150 08556 08000 07350 06700 06000 05250 04556 03850 03100 .02400 .01650 ,00850 .60006 ,00900 0 00000 00250 00500 61006 01500 02000 03000 04000 06000 08006 10000 12500 15000 17500 20000 Z_501, 25000 27500 30000 32500 35000 37506 40000 42500 45000 47500 50000 52506 55000 57500 60000 62500 65000 67506 70000 72500 75000 7.7500 .80000 .82501; .85000 .87500 ,90000 .92500 ,95000 .97506 1.00000 ORI_NAL PAGE 19 OF POOR QUALITY 'iI 0 00000 - 00700 - 01i-50 - 0170rl - 02050 - 02300 - 02700 - 02950 - 03200 - 03400 - 03500 - 03650 - 03750 - 03800 - 03800 - 03800 - 03750 - 03700 - 03G50 - 03600 03550 { )._:,500 "% -.03450 - 03300 •- 03150 03050 02950 - 02800 - 02650 02450 02200 -.02000 -.01750 -.01500 --.01300 -,01100 - 00950 - 00750 - 00550 - 06400 - 00300 - 00200 - 00250 - 00350 - oo55n - 06800 - 0 Ir)O0 59 ®, /
i 60 _IOINJU,, pAOli Ill _I p_OR OUAUTY TABLE 4.- Continued (C) Var_.Eze winglet tip (x/c) U (z/c)u (x/c) L (z/c) L 0.00000 00430 00710 01430 02860 04290 05710 08570 11430 17140 -2660 • ,"8_,70 ,34290 .40000 .45710 .51z,30 ,571 40 ,62860 .68570 74290 80000 85710 91430 97140 1 00000 00000 01570 02140 02860 03710 04430 05000 06140 07140 085_0 09860 10710 11290 11930 11930 11930 .11000 .10140 .09140 .07710 .05860 .04060 ,01860 ,00430 .01430 0 00000 00430 00710 01430 02860 04290 05710 08570 11430 17140 22860 28570 34290 40000 45710 51430 57140 62860 68570 74290 80000 85710 91430 97140 1 O0000 0.00000 -,01570 -.02140 - 0300(; .- 03710 - 04140 - 04290 - 04570 - 04860 - 65000 - 05290 .................. =..05140 - 04860 - 04570 - 04290 - 63570 02860 - 02290 - 01860 - 01.570 - 01430 -,O129O -,01140 -,01290 -.01430 ®
Page 1 and 2:
3 I" NASA Technical Paper 225.6 Jun
Page 3 and 4:
m_ Use of trademarks or names of ma
Page 5 and 6:
'*l ,_5 7,,4+-. + + +_''_m'_T _+_
Page 7 and 8:
This report presents the results of
Page 9 and 10:
i Rc R 0 r S s T t/c U.s. V V c V i
Page 11 and 12:
_i._J •J k_ Reynolds number_, Mat
Page 13 and 14: I installation of an outboard leadi
Page 15 and 16: ii, p,. _2 ,'ZI Reynolds numberof-1
Page 17 and 18: L r ...... _ 11 , Airplane level-fl
Page 19 and 20: I',/ L figures 20 to 23. The reduct
Page 21 and 22: i 7: region of the airfoil. Further
Page 23 and 24: k! k K , " _Rmlmlllll_lNiiillnp v 9
Page 25 and 26: k.L" F i' N apparent small velocity
Page 27 and 28: _T"_T _ 7] I _ - _'_' T occurred on
Page 29 and 30: shape as an indication of transitio
Page 31 and 32: level. Analysis shows that at a mor
Page 33 and 34: i< 1 11 APPENDIX SURFACE WAVINESS O
Page 35 and 36: 3O Airplane VariEze in flight Long-
Page 37 and 38: Relative gauge- reading, in. 8O 80
Page 39 and 40: k' F' &. _', b ,_ .-wT 7- Relative
Page 41 and 42: i ;:7" --..i iI m :, r, •_ $ 36 A
Page 43 and 44: 38 BO x 10-.3 70 BO 5O 4O 3O 2O I0
Page 45 and 46: 70 x 10-3 B0 l l 50 I. 4o \;,_.=.\
Page 47 and 48: 42 Relative gauge 6O 50 reading, in
Page 49 and 50: 6O 50 40 30 20 iO 0 B0 50 40 Relati
Page 51 and 52: L!I L C 46 70 BO 50 4O 30 20 iO 0 R
Page 53 and 54: _I 48 REFERENCES I. Loftin, Laurenc
Page 55 and 56: _i _ 30. Braslow, Albert L.; and Kn
Page 57 and 58: [ 52 m v ._ :_ ._ v o = "_" II x °
Page 59 and 60: i" 54 e3 ! URIGINAL PAt_E Ig OF POO
Page 61 and 62: 2, r"-" r. .! . 7L I g _ , _. ,,9®
Page 63: 58 OI_IGINAL PAGE-Ig _F POOR QUALrT
Page 67 and 68: 62 TABLE 5.- PHYSICAL CIIARACTERIST
Page 69 and 70: 64 (x/e)u 0 0000O 00000 00196 00644
Page 71 and 72: !+ • + _;+ TABLE 7.- +PHYSICAL CH
Page 73 and 74: Z :c 68 (x/c)i_ 000000 00288 00575
Page 75 and 76: TABLE 10.- PHYSICAL CHARACTERISTICS
Page 77 and 78: ;_ i_ "_. 72 TABLE12.- PHYSICALCHAR
Page 79 and 80: _r i ..............................
Page 81 and 82: I 76 >- ,----7"I __ -_---qnlmwmnm_-
Page 83 and 84: ; , L i L_ _, k "/B // I _JRIGINALP
Page 85 and 86: °?. ORIGINAl.. PAGE IB OF pOOR OUA
Page 87 and 88: ORIGINAL PAGE 18 OF POOR QUALITY ®
Page 89 and 90: i _NAt, I'VE IS OF POOROUAUTY
Page 91 and 92: il_ _. 86 ! ORIGINAL PAGE Ig OF =PO
Page 93 and 94: If 'i " F t: i k"!.. ORIGINAL PAaE
Page 95 and 96: 9O ORI_NAL PAGE Ig OF POOR OI,JAL.I
Page 97 and 98: 92 (x/c) t = 55 percent Z ORIGINAL
Page 99 and 100: _4 . OR/a/_,_ PAQE 18 OF POOR quALr
Page 101 and 102: 96 i ] i i!......J J ! i i ( I i I
Page 103 and 104: 98 _ z_ tt // /V (_ _, ORI_K/D,L, p
Page 105 and 106: loo 0 oi.._ L F-. 0 II ÷ 0 ORIGINA
Page 107 and 108: ii, _..:j ._t _ ....... 102 ORIGINA
Page 109 and 110: 7, I!/ , T & / .J l i CL 1.2 1.0 0.
Page 111 and 112: i ORIGINAL PAGE |_] OF POOR QUALITY
Page 113 and 114: ORIGINAL PAGE IR OF POOR OUALITY I
Page 115 and 116:
ORIQINAL PAGF..i_ OF POOR QUALITY 3
Page 117 and 118:
112 0 e.o ORIGINAL PAGE IS OF POOR
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i., L-.. _A / 114 ORIGINAL PA(.._._
Page 121 and 122:
116 .p 0 × o II \ II co H ¢) °¢
Page 123 and 124:
_i-_ , ORIGI/NAL PAGE _9 OF POOR QU
Page 125 and 126:
_20 i_' POOR QUALI'_( o_ ¢N I O 0
Page 127 and 128:
122 OP POORQuALrry I ¢; _k _J o_ o
Page 129 and 130:
i _. / ,p. _'- CO ¢t_ 4J ORIGINAL
Page 131 and 132:
126 ORI_NAL PAGF. I_ OF POOR QUALIT
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L'_::; : • 128 ORi_NAI.,PAGEIB OF
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130 _e8 , • , ".4 Cp 0 .4 .8 z/c
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SECTION DRAG COEFFIClENT, 132 Cd .0
Page 139 and 140:
I ,,, z/c 134 .O6 .05 .04 .03 .02 .
Page 141 and 142:
i.- _ l! I' h . MINIGLOVE NLF GLOVE
Page 143 and 144:
__ F_ Experimental transition ,| OR
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