NASA Technical Paper 2256 - CAFE Foundation

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,'1 _Y ORIGINAL PAGE Ig OF POOR QUALITY I / t / ! I ? / / / / / ! I / ! / t/ / / / / / ! c_ Lt3 F-- I I (1) (U .C e.-I O 4,-I. ¢1 .r-I e-( r.-I 4-) r_ c_ 0 .,-t I 1 II)
°?. ORIGINAl.. PAGE IB OF pOOR OUALI'I"Y PROPELLER PLANE--_ If/ Figure 7.- Planview of Biplane Racer used in natural laminar flow-flight experiments. 8O l .a, T ,E t e
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3 I" NASA Technical Paper 225.6 Jun
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m_ Use of trademarks or names of ma
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'*l ,_5 7,,4+-. + + +_''_m'_T _+_
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This report presents the results of
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i Rc R 0 r S s T t/c U.s. V V c V i
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_i._J •J k_ Reynolds number_, Mat
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I installation of an outboard leadi
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ii, p,. _2 ,'ZI Reynolds numberof-1
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L r ...... _ 11 , Airplane level-fl
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I',/ L figures 20 to 23. The reduct
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i 7: region of the airfoil. Further
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k! k K , " _Rmlmlllll_lNiiillnp v 9
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k.L" F i' N apparent small velocity
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_T"_T _ 7] I _ - _'_' T occurred on
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shape as an indication of transitio
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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
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Page 47 and 48: 42 Relative gauge 6O 50 reading, in
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Page 53 and 54: _I 48 REFERENCES I. Loftin, Laurenc
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Page 59 and 60: i" 54 e3 ! URIGINAL PAt_E Ig OF POO
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Page 63 and 64: 58 OI_IGINAL PAGE-Ig _F POOR QUALrT
Page 65 and 66: i 60 _IOINJU,, pAOli Ill _I p_OR OU
Page 67 and 68: 62 TABLE 5.- PHYSICAL CIIARACTERIST
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Page 71 and 72: !+ • + _;+ TABLE 7.- +PHYSICAL CH
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Page 75 and 76: TABLE 10.- PHYSICAL CHARACTERISTICS
Page 77 and 78: ;_ i_ "_. 72 TABLE12.- PHYSICALCHAR
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Page 87 and 88: ORIGINAL PAGE 18 OF POOR QUALITY ®
Page 89 and 90: i _NAt, I'VE IS OF POOROUAUTY
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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
Page 119 and 120: 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
Page 133 and 134: 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
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NASA Technical Paper 2256 - CAFE Foundation

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