tabla de lab-aerodinamica

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  • 7/24/2019 Tabla de Lab-Aerodinamica

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    VELOCIDAD : 80Km/H (22,22m/s) a H= 0,031m

    N h1(m) P(Pa) !(m) "(m)

    1 0.054 -529.74 3.5 28.5 0.019104 0.3

    2 0.059 -578.79 3.5 15.5 0.017303 0.3

    3 0.059 -578.79 3.5 10.5 0.016344 0.3

    4 0.044 -431.64 3.5 5.5 0.016168 0.3

    5 0.032 -313.92 3.5 2.5 0.016522 0.3

    6 0.032 -313.92 3.5 -0.5 0.024754 0.3

    7 0.022 -215.82 3.5 8.5 0.033074 0.3

    8 0.019 -186.39 3.5 10.5 0.033066 0.3

    9 0.016 -156.96 3.5 12.5 0.033113 0.3

    10 0.007 -68.97 3.5 14.5 0.033381 0.3

    11 0.005 -49.05 3.5 29.5 0.017943 0.3

    12 0.009 -88.29 3.5 15.5 0.016903 0.3

    13 0.007 -68.67 3.5 11.5 0.016179 0.3

    14 0.014 -137.34 3.5 7.5 0.016076 0.3

    15 0.014 -137.34 3.5 5.5 0.016522 0.3

    16 0.008 -78.48 3.5 -2.5 0.024763 0.3

    17 0.01 -98.1 3.5 0.5 0.033098 0.3

    18 0.011 -107.91 3.5 1.5 0.032985 0.3

    19 0.006 -58.86 3.5 2.5 0.033005 0.3

    20 0.003 -29.43 3.5 4.5 0.033181 0.3

    #

    VELOCIDAD : 1$0Km/H (%1,&'m/s) a H= 0,108%m

    N h3(m) P(Pa) !(m) "(m)

    1 0.099 -971.19 3.5 28.5 0.019104 0.3

    2 0.11 -1079.1 3.5 15.5 0.017303 0.3

    3 0.111 -1088.91 3.5 10.5 0.016344 0.3

    4 0.086 -843.66 3.5 5.5 0.016168 0.3

    5 0.059 -578.79 3.5 2.5 0.016522 0.3

    6 0.058 -568.98 3.5 -0.5 0.024754 0.3

    7 0.041 -402.21 3.5 8.5 0.033074 0.3

    8 0.033 -323.73 3.5 10.5 0.033066 0.3

    9 0.027 -264.87 3.5 12.5 0.033113 0.3

    10 0.012 -117.72 3.5 14.5 0.033381 0.3

    11 0.011 -107.91 3.5 29.5 0.017943 0.3

    12 0.017 -166.77 3.5 15.5 0.016903 0.3

    13 0.008 -78.48 3.5 11.5 0.016179 0.314 0.029 -284.49 3.5 7.5 0.016076 0.3

    15 0.026 -255.06 3.5 5.5 0.016522 0.3

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    16 0.017 -166.77 3.5 -2.5 0.024763 0.3

    17 0.019 -186.39 3.5 0.5 0.033098 0.3

    18 0.023 -225.63 3.5 1.5 0.032985 0.3

    19 0.013 -127.53 3.5 2.5 0.033005 0.3

    20 0.01 -98.1 3.5 4.5 0.033181 0.3

    #

    MOMENTOS DE FUERZA par

    E*+A E*+A - DISTANCIA X(m) DISTANCIA Y(m) MO

    1 1.4484974932 -2.668077126 0.013841 0.0165 0.0

    2 0.8027866381 -2.895079358 0.018839 0.033 0.0

    3 0.5170695939 -2.790246019 0.022126 0.0495 0.0

    4 0.2005694336 -2.083786611 0.024182 0.0659 0.

    5 0.067840548 -1.554419896 0.025586 0.0825 0.0

    6 0.0202817245 -2.330999581 0.02632 0.0989 0.0

    7 -0.3165002804 -2.117853703 0.026183 0.132 -0.0

    8 -0.3368789673 -1.817889136 0.024421 0.165 -0.0

    9 -0.3374162779 -1.52211539 0.021564 0.198 -0.0

    10 -0.1728787736 -0.668653379 0.017792 0.231 -0.0

    11 0.130008985 0.2297863925 0.010028 0.0165 0.0

    12 0.1196280481 0.4314131257 0.012602 0.033 0.0

    13 0.0664274033 0.3266041771 0.013739 0.0495 0.0

    14 0.0864384174 0.6566670272 0.014131 0.0659 0.0

    15 0.0652148387 0.6775399686 0.014144 0.0825 0.0

    16 0.0254196751 0.5824370519 0.013857 0.0989 0.0

    17 -0.008474445 0.9739767326 0.012808 0.132 -0.0

    18 -0.0278701909 1.0673962756 0.01133 0.165 -0.0

    19 -0.0254101798 0.5822194877 0.009483 0.198 -0.0

    20 -0.0229676758 0.2920468883 0.007439 0.231 -0.0

    2.301'8&008$ 1%.&20330'28 # 0.0

    DISTANCIAS DE PERFIL X

    X Y 1.3841

    1 20 1.65 1.8839

    2 3.3 2.2126

    3 4.95 2.4182

    4 6.59 2.5586

    5 8.25 2.632

    6 9.89 2.6183

    7 13.2 2.4421

    8 16.5 2.1564

  • 7/24/2019 Tabla de Lab-Aerodinamica

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    9 19.8 1.7792

    10 23.1 1.0028

    11 1.2602

    12 1.3739

    13 1.4131

    14 1.4144

    15 1.3857

    16 1.2808

    17 1.133

    18 0.9483

    19 0.7439

    20

    MOMENTOS DE FUERZA par

    E*+A E*+A - DISTANCIA X(m) DISTANCIA Y(m) MO

    1 2.1861582536 -4.026820107 0.013841 0.0165 0.0

    2 1.2654094466 -4.563430175 0.018839 0.033 0.0

    3 0.8150419023 -4.398184404 0.022126 0.0495 0.0

    4 0.3282045278 -3.409832636 0.024182 0.0659 0.0

    5 0.118720959 -2.720234818 0.025586 0.0825 0.0

    6 0.0354930179 -4.079249266 0.02632 0.0989 0.0

    7 -0.5179095497 -3.465578786 0.026183 0.132 -0.0

    8 -0.5372333005 -2.899054781 0.024421 0.165 -0.0

    9 -0.5272129342 -2.378305297 0.021564 0.198 -0.0

    10 -0.3319588283 -1.283936643 0.017792 0.231 -0.0

    11 0.2860197671 0.5055300636 0.010028 0.0165 0.0

    12 0.2126720856 0.7669566679 0.012602 0.033 0.0

    13 0.0854066614 0.4199196562 0.013739 0.0495 0.0

    14 0.1605284895 1.219524479 0.014131 0.0659 0.0

    15 0.1211132719 1.2582885131 0.014144 0.0825 0.0

    16 0.0540168097 1.2376787353 0.013857 0.0989 0.0

    17 -0.0161014455 1.8505557919 0.012808 0.132 -0.0

    18 -0.0511798051 1.9601277062 0.01133 0.165 -0.0

    19 -0.0564105993 1.2925272627 0.009483 0.198 -0.0

    20 -0.0689030275 0.876140665 0.007439 0.231 -0.0

    3.5618757023 -21.83737737 # 0.0

    MOMENTOS DE FUERZA par

    E*+A E*+A - DISTANCIA X(m) DISTANCIA Y(m) MO1 2.6555787375 -4.891474732 0.013841 0.0165 0.0

    2 1.4967208508 -5.397605583 0.018839 0.033 0.0

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    3 0.9727919479 -5.249445901 0.022126 0.0495 0.0

    4 0.3920220749 -4.072855648 0.024182 0.0659 0.0

    5 0.1250810104 -2.865961683 0.025586 0.0825 0.0

    6 0.0367606257 -4.22493674 0.02632 0.0989 0.0

    7 -0.5898414316 -3.946909173 0.026183 0.132 -0.0

    8 -0.5851055748 -3.157386395 0.024421 0.165 -0.0

    9 -0.5693899689 -2.568569721 0.021564 0.198 -0.0

    10 -0.295074514 -1.141277016 0.017792 0.231 -0.0

    11 0.2860197671 0.5055300636 0.010028 0.0165 0.0

    12 0.2259640909 0.8148914597 0.012602 0.033 0.0

    13 0.0759170323 0.3732619166 0.013739 0.0495 0.0

    14 0.1790510075 1.360238842 0.014131 0.0659 0.0

    15 0.1211132719 1.2582885131 0.014144 0.0825 0.0

    16 0.0540168097 1.2376787353 0.013857 0.0989 0.0

    17 -0.0161014455 1.8505557919 0.012808 0.132 -0.0

    18 -0.0582740355 2.2318285763 0.01133 0.165 -0.0

    19 -0.0550553897 1.2614755567 0.009483 0.198 -0.0

    20 -0.0765589195 0.9734896278 0.007439 0.231 -0.0

    4.3756359472 -25.64918351 # 0.0

    MOMENTOS DE FUERZA par

    E*+A E*+A - DISTANCIA X(m) DISTANCIA Y(m) MO

    1 3.1920592905 -5.879651445 0.013841 0.0165 0.0

    2 1.7552453614 -6.329919275 0.018839 0.033 0.0

    3 1.1393058849 -6.147999704 0.022126 0.0495 0.0

    4 0.4467228295 -4.641161088 0.024182 0.0659 0.0

    5 0.1420411474 -3.254566658 0.025586 0.0825 0.0

    6 0.0418310568 -4.807686635 0.02632 0.0989 0.0

    7 -0.6617733135 -4.42823956 0.026183 0.132 -0.0

    8 -0.6560274627 -3.540099897 0.024421 0.165 -0.0

    9 -0.632655521 -2.853966357 0.021564 0.198 -0.0

    10 -0.295074514 -1.141277016 0.017792 0.231 -0.0

    11 0.156010782 0.275743671 0.010028 0.0165 0.0

    12 0.1860880749 0.6710870844 0.012602 0.033 0.0

    13 0.0284688871 0.1399732187 0.013739 0.0495 0.0

    14 0.1852251802 1.4071436297 0.014131 0.0659 0.0

    15 0.1164550692 1.2098928011 0.014144 0.0825 0.0

    16 0.0476618909 1.0920694724 0.013857 0.0989 0.0

    17 -0.015254001 1.7531581187 0.012808 0.132 -0.0

    18 -0.0557403817 2.1347925513 0.01133 0.165 -0.0

    19 -0.0508203597 1.1644389754 0.009483 0.198 -0.0

    20 -0.0689030275 0.876140665 0.007439 0.231 -0.05.0008668737 -32.30012745 # 0.0

  • 7/24/2019 Tabla de Lab-Aerodinamica

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    SENO() COS()

    -

    1.4484974932 -2.6680771264 0.4771 0.8788 58

    0.8027866381 -2.8950793582 0.2672 0.9636 71

    0.5170695939 -2.7902460194 0.1822 0.9832 76

    0.2005694336 -2.0837866107 0.0958 0.9953 81

    0.067840548 -1.5544198961 0.0436 0.999 84

    0.0202817245 -2.3309995807 -0.0087 0.9999 87

    -0.31650028 -2.1178537028 0.1478 0.989 85

    -0.336878967 -1.8178891364 0.1822 0.9832 83

    -0.337416278 -1.5221153903 0.2164 0.9762 81

    -0.172878774 -0.668653379 0.2503 0.9681 79

    0.130008985 0.2297863925 0.4924 0.8703 64

    0.1196280481 0.4314131257 0.2672 0.9636 78

    0.0664274033 0.3266041771 0.1993 0.9799 82

    0.0864384174 0.6566670272 0.1305 0.9914 86

    0.0652148387 0.6775399686 0.0958 0.9953 88

    0.0254196751 0.5824370519 -0.0436 0.999 89

    -0.008474445 0.9739767326 0.0087 0.9999 86

    -0.027870191 1.0673962756 0.0261 0.9996 85

    -0.02541018 0.5822194877 0.0436 0.999 84

    -0.022967676 0.2920468883 0.0784 0.9969 82

    2.301'8&008$ 1%.&20330'28

    -

    2.6555787375 -4.8914747317 0.4771 0.8788

    1.4967208508 -5.3976055831 0.2672 0.9636

    0.9727919479 -5.249445901 0.1822 0.9832

    0.3920220749 -4.0728556482 0.0958 0.9953

    0.1250810104 -2.8659616835 0.0436 0.999

    0.0367606257 -4.2249367401 -0.0087 0.9999

    -0.589841432 -3.9469091733 0.1478 0.989

    -0.585105575 -3.1573863949 0.1822 0.9832

    -0.569389969 -2.5685697212 0.2164 0.9762

    -0.295074514 -1.1412770157 0.2503 0.9681

    0.2860197671 0.5055300636 0.4924 0.8703

    0.2259640909 0.8148914597 0.2672 0.9636

    0.0759170323 0.3732619166 0.1993 0.97990.1790510075 1.360238842 0.1305 0.9914

    0.1211132719 1.2582885131 0.0958 0.9953

  • 7/24/2019 Tabla de Lab-Aerodinamica

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    0.0540168097 1.2376787353 -0.0436 0.999

    -0.016101446 1.8505557919 0.0087 0.9999

    -0.058274035 2.2318285763 0.0261 0.9996

    -0.05505539 1.2614755567 0.0436 0.999

    -0.076558919 0.9734896278 0.0784 0.9969

    %.3'$&3$%'2 2$.&%183$0$

    H1

    ENTO(Fx) MOMENTO(F!)

    00486538 -0.0440232726

    51236975 -0.0955376188

    14406818 -0.138117178

    0485017 -0.1373215376

    17357683 -0.1282396414

    00533815 -0.2305358585

    82869268 -0.2795566888

    82269213 -0.2999517075

    72760446 -0.3013788473

    30758591 -0.1544589305

    13037301 0.0037914755

    15075527 0.0142366331

    09126461 0.0161669068

    12214613 0.0432743571

    09223987 0.0558970474

    03522404 0.0576030244

    01085407 0.1285649287

    03157693 0.1761203855

    02409647 0.1152794586

    01708565 0.0674628312

    22$032& 1.130'2%2328

    DS

    1.9104

    1.7303

    1.6344

    1.6168

    1.6522

    2.4754

    3.3074

    3.3066

    3.3113

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    3.3381

    1.7943

    1.6903

    1.6179

    1.6076

    1.6522

    2.4763

    3.3098

    3.2985

    3.3005

    3.3181

    H2

    ENTO(Fx) MOMENTO(F!)

    02586164 -0.0664425318

    38390486 -0.1505931958

    80336171 -0.217710128

    79366419 -0.2247079707

    30375945 -0.2244193725

    09341762 -0.4034377524

    35604257 -0.4574563998

    31197744 -0.4783440388

    13688197 -0.4709044489

    59062115 -0.2965893644

    28682062 0.008341246

    26800936 0.02530957

    11734021 0.020786023

    22684281 0.0803666632

    17130261 0.1038088023

    07485109 0.1224064269

    02062273 0.2442733645

    05798672 0.3234210715

    05349417 0.255920398

    05125696 0.2023884936

    '02$2%& 1.&03$831%3

    H3

    ENTO(Fx) MOMENTO(F!)67558653 -0.0807093331

    81967241 -0.1781209842

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    15239946 -0.2598475721

    94798778 -0.2684011872

    32003227 -0.2364418389

    09675397 -0.4178462436

    54438182 -0.5209920109

    42888632 -0.5209687552

    22783253 -0.5085768048

    52499658 -0.2636349906

    28682062 0.008341246

    28475995 0.0268914182

    10430241 0.0184764649

    25301698 0.0896397397

    17130261 0.1038088023

    07485109 0.1224064269

    02062273 0.2442733645

    06602448 0.3682517151

    05220903 0.2497721602

    05695218 0.224876104

    2&$$80%2 1.'88022'8&

    H4

    ENTO(Fx) MOMENTO(F!)

    41812926 -0.0970142488

    30670674 -0.2088873361

    25208282 -0.3043259853

    08026515 -0.3058525157

    36342648 -0.2685017492

    11009934 -0.4754802082

    73272107 -0.584527622

    60208467 -0.584116483

    36425837 -0.5650853387

    52499658 -0.2636349906

    15644761 0.0045497706

    23450819 0.0221458738

    00391134 0.0069286743

    02617417 0.0927307652

    16471405 0.0998161561

    06604508 0.1080056708

    01953732 0.2314168717

    06315385 0.352240771

    04819295 0.2305589171

    05125696 0.202388493631$823%$ 2.30&&%%$13$

  • 7/24/2019 Tabla de Lab-Aerodinamica

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    VELOCIDAD : 120Km/H (33,33m/s) a H= 0,0&m

    N h2(m) P(Pa) !(m) "(m)

    1 0.0815 -799.515 3.5 28.5 0.019104 0.3 2.1861582536

    2 0.093 -912.33 3.5 15.5 0.017303 0.3 1.2654094466

    3 0.093 -912.33 3.5 10.5 0.016344 0.3 0.8150419023

    4 0.072 -706.32 3.5 5.5 0.016168 0.3 0.3282045278

    5 0.056 -549.36 3.5 2.5 0.016522 0.3 0.118720959

    6 0.056 -549.36 3.5 -0.5 0.024754 0.3 0.0354930179

    7 0.036 -353.16 3.5 8.5 0.033074 0.3 -0.51790955

    8 0.0303 -297.243 3.5 10.5 0.033066 0.3 -0.5372333

    9 0.025 -245.25 3.5 12.5 0.033113 0.3 -0.527212934

    10 0.0135 -132.435 3.5 14.5 0.033381 0.3 -0.331958828

    11 0.011 -107.91 3.5 29.5 0.017943 0.3 0.2860197671

    12 0.016 -156.96 3.5 15.5 0.016903 0.3 0.2126720856

    13 0.009 -88.29 3.5 11.5 0.016179 0.3 0.0854066614

    14 0.026 -255.06 3.5 7.5 0.016076 0.3 0.1605284895

    15 0.026 -255.06 3.5 5.5 0.016522 0.3 0.1211132719

    16 0.017 -166.77 3.5 -2.5 0.024763 0.3 0.0540168097

    17 0.019 -186.39 3.5 0.5 0.033098 0.3 -0.016101446

    18 0.0202 -198.162 3.5 1.5 0.032985 0.3 -0.051179805

    19 0.01332 -130.6692 3.5 2.5 0.033005 0.3 -0.056410599

    20 0.009 -88.29 3.5 4.5 0.033181 0.3 -0.068903028

    # 3.$&18'$'023

    VELOCIDAD : 180Km/H ($0m/s) a H= 0,1$&m

    N h%(m) P(Pa) !(m) "(m)

    1 0.119 -1167.39 3.5 28.5 0.019104 0.3 3.1920592905

    2 0.129 -1265.49 3.5 15.5 0.017303 0.3 1.7552453614

    3 0.13 -1275.3 3.5 10.5 0.016344 0.3 1.1393058849

    4 0.098 -961.38 3.5 5.5 0.016168 0.3 0.4467228295

    5 0.067 -657.27 3.5 2.5 0.016522 0.3 0.1420411474

    6 0.066 -647.46 3.5 -0.5 0.024754 0.3 0.0418310568

    7 0.046 -451.26 3.5 8.5 0.033074 0.3 -0.661773313

    8 0.037 -362.97 3.5 10.5 0.033066 0.3 -0.656027463

    9 0.03 -294.3 3.5 12.5 0.033113 0.3 -0.632655521

    10 0.012 -117.72 3.5 14.5 0.033381 0.3 -0.295074514

    11 0.006 -58.86 3.5 29.5 0.017943 0.3 0.156010782

    12 0.014 -137.34 3.5 15.5 0.016903 0.3 0.1860880749

    13 0.003 -29.43 3.5 11.5 0.016179 0.3 0.028468887114 0.03 -294.3 3.5 7.5 0.016076 0.3 0.1852251802

    15 0.025 -245.25 3.5 5.5 0.016522 0.3 0.1164550692

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    16 0.015 -147.15 3.5 -2.5 0.024763 0.3 0.0476618909

    17 0.018 -176.58 3.5 0.5 0.033098 0.3 -0.015254001

    18 0.022 -215.82 3.5 1.5 0.032985 0.3 -0.055740382

    19 0.012 -117.72 3.5 2.5 0.033005 0.3 -0.05082036

    20 0.009 -88.29 3.5 4.5 0.033181 0.3 -0.068903028

    # $.0008&&8'3'

    D2=

    D1= 0.07729316

    7.72931627

    D3= 0.07013098 D4=

    7.01309762

    H1 H2

    -0.48863686

    0.07688393

    H3 H4

    -0.24360447

    0.04155783

    CL" CL"

    CD"

    CD"

    CL" CL"

    CD" CD"

  • 7/24/2019 Tabla de Lab-Aerodinamica

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  • 7/24/2019 Tabla de Lab-Aerodinamica

    12/16

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    -

    -4.026820107 0.4771 0.8788

    -4.563430175 0.2672 0.9636

    -4.398184404 0.1822 0.9832

    -3.409832636 0.0958 0.9953

    -2.720234818 0.0436 0.999

    -4.079249266 -0.0087 0.9999

    -3.465578786 0.1478 0.989

    -2.899054781 0.1822 0.9832

    -2.378305297 0.2164 0.9762

    -1.283936643 0.2503 0.9681

    0.5055300636 0.4924 0.8703

    0.7669566679 0.2672 0.9636

    0.4199196562 0.1993 0.9799

    1.219524479 0.1305 0.9914

    1.2582885131 0.0958 0.9953

    1.2376787353 -0.0436 0.999

    1.8505557919 0.0087 0.9999

    1.9601277062 0.0261 0.9996

    1.2925272627 0.0436 0.999

    0.876140665 0.0784 0.9969

    21.83'3''3'2

    -

    -5.879651445 0.4771 0.8788

    -6.329919275 0.2672 0.9636

    -6.147999704 0.1822 0.9832

    -4.641161088 0.0958 0.9953

    -3.254566658 0.0436 0.999

    -4.807686635 -0.0087 0.9999

    -4.42823956 0.1478 0.989

    -3.540099897 0.1822 0.9832

    -2.853966357 0.2164 0.9762

    -1.141277016 0.2503 0.9681

    0.275743671 0.4924 0.8703

    0.6710870844 0.2672 0.9636

    0.1399732187 0.1993 0.97991.4071436297 0.1305 0.9914

    1.2098928011 0.0958 0.9953

  • 7/24/2019 Tabla de Lab-Aerodinamica

    14/16

    1.0920694724 -0.0436 0.999

    1.7531581187 0.0087 0.9999

    2.1347925513 0.0261 0.9996

    1.1644389754 0.0436 0.999

    0.876140665 0.0784 0.9969

    32.30012'%%&%

    0.0734329547

    7.3432954726

    0.0714128611

    7.1412861059

    0.0528770046

    -0.324181751

    0.094

    -0.213070311

    0.0329886085

    0.014

  • 7/24/2019 Tabla de Lab-Aerodinamica

    15/16

  • 7/24/2019 Tabla de Lab-Aerodinamica

    16/16