1 Relative gauge reading, in. 30 x 10 -3 • y, 2O r I0 0 3O 2O iO 0 3O 2Q _O 0 •, 0 .I I -/1 Aw v APPENDIX I \\t : V; _./ V / I t A ^ /I L_ J 1 ORIGINAL PAGE 18 OF POOR QUALITY 1 I I 1 _ n = 0.75 -- c = 22.5 in. | I I ! q : 0.85 c = 19.9 in,-- ]]I] ll-ll Data ..... Nine-point avg A '¸ , .... t} n = 0.95 -- c = 17.3 in. ,_. ' j ': 2 4 6 B iO 12 14 IB IB 20 22 24 2B 2B 30 32 34 S8 3B 40 Distance along surface from L.E., in, -- (a) Concluded. Figure A2.- continued. • .,._ _,.- ..,--.. _,,_ ._/_,, .......... .;., .._.............. ................... __:..... :,.._
k' F' &. _', b ,_ .-wT 7- Relative gauge reading, in. ' 34 _ BO 50 4O BO 20 I0 0 BO BO 40 BO. 20 I0 o BO -3 -,, ,, ,, %---- APPENDIX " \ _ :k ',,:_:./ \, ,,/ %. \''_" ";'_1' :1 I;_',r \" IV H all .... ,,, 211 .. t0 0 0 ,,-- , , ORIGINAL PAGE 19 OF POOR QUAUW n = 0.25 c = 16.8 in. - l,, j .... .i '_ _ u ,,.; ' L I I ,n = 0.55 c = 12.9 in. I I.... Data ..... Nine-point avg .I I .... I .... 2 4 B B t0 t2 i4 tB Distance along surface from L,E,, in, (b) Upper surf&ce of right winglet. Figure A2.- Continued. I I n : 0.80 - • c : 9.6 in." I i8 20
- 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: Relative gauge- reading, in. 8O 80
- 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 and 64: 58 OI_IGINAL PAGE-Ig _F POOR QUALrT
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- 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
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- Page 87 and 88: ORIGINAL PAGE 18 OF POOR QUALITY ®
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i _NAt, I'VE IS OF POOROUAUTY
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il_ _. 86 ! ORIGINAL PAGE Ig OF =PO
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If 'i " F t: i k"!.. ORIGINAL PAaE
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9O ORI_NAL PAGE Ig OF POOR OI,JAL.I
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92 (x/c) t = 55 percent Z ORIGINAL
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_4 . OR/a/_,_ PAQE 18 OF POOR quALr
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96 i ] i i!......J J ! i i ( I i I
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98 _ z_ tt // /V (_ _, ORI_K/D,L, p
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loo 0 oi.._ L F-. 0 II ÷ 0 ORIGINA
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ii, _..:j ._t _ ....... 102 ORIGINA
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7, I!/ , T & / .J l i CL 1.2 1.0 0.
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i ORIGINAL PAGE |_] OF POOR QUALITY
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ORIGINAL PAGE IR OF POOR OUALITY I
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ORIQINAL PAGF..i_ OF POOR QUALITY 3
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112 0 e.o ORIGINAL PAGE IS OF POOR
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i., L-.. _A / 114 ORIGINAL PA(.._._
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116 .p 0 × o II \ II co H ¢) °¢
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_i-_ , ORIGI/NAL PAGE _9 OF POOR QU
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_20 i_' POOR QUALI'_( o_ ¢N I O 0
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122 OP POORQuALrry I ¢; _k _J o_ o
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i _. / ,p. _'- CO ¢t_ 4J ORIGINAL
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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
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I ,,, z/c 134 .O6 .05 .04 .03 .02 .
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i.- _ l! I' h . MINIGLOVE NLF GLOVE
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__ F_ Experimental transition ,| OR