Vistas del avin Aero Commander 500

Datos de la aeronave

DatoALAEMPENAJE HORIZONTAL

PERFILNACA 23012NACA 0012

Cuerda de raz (m)2.411.4

Cuerda de punta (m)0.7620.56

Alargamiento 9.45

Conicidad0.31620.4

Superficie alar (m2)23.695.92

Envergadura (m)14.9345 5.1

Torcimiento ()1.50

Significado de las columnasColumnaSignificado

1ngulo de ataque del fuselaje

2ngulo de ataque del ala

3Coeficiente de levantamiento del ala

4Coeficiente de resistencia al avance del perfil que conforma el ala.

5Coeficiente de resistencia al avance inducida del ala

6Coeficiente de resistencia al avance del ala

7Desviacin de la estela producida por el ala

8ngulo de ataque del empenaje horizontal

9Coeficiente de levantamiento del empenaje horizontal

10Coeficiente de levantamiento del empenaje horizontal debido a la superficie alar

11Coeficiente de resistencia al avance del perfil que conforma al empenaje horizontal

12Coeficiente de resistencia al avance inducida del empenaje horizontal

13Coeficiente de resistencia al avance del empenaje horizontal

14Coeficiente de resistencia al avance del empenaje horizontal referido a la superficie alar

15Coeficiente de levantamiento total sin aletas extendidas (avin limpio)

16Coeficiente de resistencia parsita que genera el empenaje vertical

17Coeficiente de resistencia al avance de las barquillas de los motores

18Coeficiente de resistencia al avance de los montantes del ala

19Coeficiente de resistencia al avance del tren de aterrizaje

20Coeficiente de resistencia al avance del fuselaje

21Coeficiente de resistencia parsita total

22Incremento en el valor del coeficiente de levantamiento referido a la superficie alar

23 Incremento en el coeficiente de resistencia al avance debido a la extensin de las aletas

24Coeficiente de levantamiento total con aletas extendidas

25Coeficiente de resistencia al avance total sin aletas y sin tren de aterrizaje

26 Coeficiente de resistencia al avance total con aletas y con tren de aterrizaje extendidos

27Coeficiente de resistencia al avance total solo con tren de aterrizaje extendido

28 Coeficiente de resistencia al avance total slo con aletas extendidas en

Tabla principal 12345678910

FACla/cdCD oa/cdCD iaCD aEHCl EH/sdCl' EH

-4-1-0.004623570.003817.3788E-070.00381074-0.01584743-3.48415257-0.19754546-0.04194299

-300.069353580.003020.000166020.003186020.23771151-2.73771151-0.14813242-0.03145158

-210.143330730.002520.000709110.003229110.49127044-1.99127044-0.09871939-0.02096017

-120.217307880.002420.001629990.004049990.74482937-1.24482937-0.04930635-0.01046876

030.291285020.002470.002928670.005398670.99838827-0.498388270.000106692.2652E-05

140.365262170.002650.004605140.007255141.25194720.24805280.049519730.01051406

250.439239320.002920.006659410.009579411.505506140.994493860.098932770.02100547

360.513216470.003280.009091480.012371481.759065071.740934930.148345810.03149688

470.587193620.003670.011901350.015571352.0126242.4873760.197758850.04198829

580.661170770.004290.015089010.019379012.266182943.233817060.247171880.0524797

690.735147920.004880.018654470.023534472.519741873.980258130.296584920.06297111

7100.809125070.005380.022597730.027977732.77330084.72669920.345997960.07346252

8110.883102220.006060.026918780.032978783.026859745.473140260.3954110.08395393

9120.957079370.006870.031617630.038487633.280418676.219581330.444824040.09444534

10131.031056510.007820.036694280.044514283.533977576.966022430.494237080.10493675

11141.105033660.009150.042148720.051298723.78753657.71246350.543650110.11542816

12151.179010810.011020.047980970.059000974.041095448.458904560.593063150.12591957

13161.252987960.013380.054191010.067571014.294654379.205345630.642476190.13641098

14171.326965110.016590.060778840.077368844.54821339.95178670.691889230.14690239

15181.400942260.021320.067744480.089064484.8017722410.69822780.741302270.1573938

16191.474919410.028930.075087910.104017915.0553311711.44466880.79071530.16788521

17201.548896560.038750.082809130.121559135.308890112.19110990.840128340.17837662

18211.622873710.056410.090908160.147318165.5624490312.9375510.889541380.18886803

19221.60.087690.08836360.17605365.484048714.01595130.960929520.2040252

20231.450.115410.072572050.187982054.9699191315.53008091.061162140.22530666

11121314151617181920

CDoEHCDiEHCD EHCD' EHCl TS/ACD' EVCD' BARCD'MCD' TACD' FUS

0.003020.002509450.005529450.00117402-0.046566560.001140.0008169400.027240470.0027

0.002520.001411060.003931060.000834640.0379020.001140.0008169400.027240470.0024

0.002420.000626680.003046680.000646870.122370560.001140.0008169400.027240470.00243

0.0024450.000156330.002601330.000552320.206839120.001140.0008169400.027240470.00245

0.002477.3197E-100.002470.000524430.291307670.001140.0008169400.027240470.00247

0.002650.000157690.002807690.000596130.375776230.001140.0008169400.027240470.00249

0.002920.00062940.00354940.000753610.460244790.001140.0008169400.027240470.0027

0.003280.001415120.004695120.000996870.544713350.001140.0008169400.027240470.0027

0.003670.002514870.006184870.001313180.629181910.001140.0008169400.027240470.00282

0.004290.003928640.008218640.001744990.713650470.001140.0008169400.027240470.003

0.004880.005656430.010536430.00223710.798119030.001140.0008169400.027240470.0036

0.005380.007698230.013078230.002776780.882587590.001140.0008169400.027240470.0039

0.006060.010054060.016114060.003421350.967056150.001140.0008169400.027240470.0036

0.006870.01272390.01959390.004160191.051524710.001140.0008169400.027240470.0042

0.007820.015707770.023527770.004995431.135993260.001140.0008169400.027240470.0045

0.009150.019005660.028155660.005978031.220461820.001140.0008169400.027240470.0051

0.011020.022617560.033637560.007141951.304930380.001140.0008169400.027240470.0054

0.013380.026543490.039923490.008476581.389398940.001140.0008169400.027240470.0057

0.016590.030783430.047373430.010058361.47386750.001140.0008169400.027240470.006

0.021320.03533740.05665740.012029541.558336060.001140.0008169400.027240470.009

0.028930.040205380.069135380.014678871.642804620.001140.0008169400.027240470.012

0.034540.045387390.079927390.016970241.727273180.001140.0008169400.027240470.015

0.038750.050883410.089633410.019031031.811741740.001140.0008169400.027240470.018

0.039870.059378190.099248190.021072441.80402520.001140.0008169400.027240470.021

0.045320.072411480.117731480.024996831.675306660.001140.0008169400.027240470.024

2122232425262728

1.05 CD' PAR CL' CD'Cl TC/ACD TS/A y TACD TC/A y TACD TC/TACD TC/A

0.033492280.89560.004662560.849033440.011236570.04313960.038477040.01589913

0.033177280.89560.004662560.9335020.009957480.041860510.037197950.01462004

0.033208780.89560.004662561.017970560.00984430.041747330.037084770.01450686

0.033229780.89560.004662561.102439120.010591620.042494650.037832090.01525418

0.033250780.89560.004662561.186907670.011933410.043836440.039173880.01659597

0.033271780.89560.004662561.271376230.013882580.045785610.041123050.01854514

0.033492280.89560.004662561.355844790.016584840.048487870.043825310.0212474

0.033492280.89560.004662561.440313350.019620170.05152320.046860640.02428273

0.033618280.89560.004662561.524781910.023262340.055165370.050502810.0279249

0.033807280.89560.004662561.609250470.027690810.059593840.054931280.03235337

0.034437280.89560.004662561.693719030.032968380.064871410.060208850.03763094

0.034752280.89560.004662561.778187590.038266320.070169350.065506790.04292888

0.034437280.89560.004662561.862656150.043596940.075499970.070837410.0482595

0.035067280.89560.004662561.947124710.050474640.082377670.077715110.0551372

0.035382280.89560.004662562.031593260.057651520.089554550.084891990.06231408

0.036012280.89560.004662562.116061820.066048570.09795160.093289040.07071113

0.036327280.89560.004662562.200530380.075229730.107132760.10247020.07989229

0.036642280.89560.004662562.284998940.08544940.117352430.112689870.09011196

0.036957280.89560.004662562.36946750.097144020.129047050.124384490.10180658

0.040107280.89560.004662562.453936060.113960830.145863860.14120130.11862339

0.043257280.89560.004662562.538404620.134713590.166616620.161954060.13937615

0.046407280.89560.004662562.622873180.157696180.189599210.184936650.16235874

0.049557280.89560.004662562.707341740.1886660.220569030.215906470.19332856

0.052707280.89560.004662562.69962520.222592850.254495880.249833320.22725541

0.055857280.89560.004662562.570906660.24159570.273498730.268836170.24625826

Graficas polares

Tabla del mtodo de Anderson para el alaEstacinYClalbClbClaCL= 1CL=1.1CL=1.2

002.411.375-0.308-0.026675770.905363450.878687690.969224031.05976038

0.21.493522.079932081.27975-0.21425-0.021500810.976367440.954866631.052503371.15014011

0.42.987041.749864161.142-0.014-0.001669961.035616761.03394681.137508471.24107015

0.64.480561.419796240.9590.12750.018744221.071839821.090584041.197768031.30495201

0.85.974081.089728320.74750.184250.035291691.088504591.123796281.232646741.34149719

0.96.720840.924694360.56150.18250.041195320.963582391.004777711.101135951.19749419

0.957.094220.842177380.429750.150.037176710.80974750.846924210.927898961.00887371

0.9757.280910.800918890.312250.091750.023911170.618658830.642569990.704435880.76630176

17.46760.75966040000000

CL=1.3CL=1.4CL=1.5CL=1.615CL del perfil

1.150296721.240833071.331369411.435486211.8

1.247776861.34541361.443050351.55533261.8

1.344631831.44819351.551755181.670851111.8

1.412135991.519319971.626503951.749765531.8

1.450347651.559198111.668048571.79322661.8

1.293852431.390210671.486568911.597380881.8

1.089848461.170823211.251797961.344918921.8

0.828167640.890033520.951899411.023045171.8

00001.8

Graficas del mtodo de Anderson para el ala

Tabla del mtodo de Anderson para el empenaje horizontalEstacinYCLaLbClbClaCL=1.1CL=1.2CL=1.23CL del perfil

001.421.333-0.225-0.0401291.089665841.158502871.267469461.300159431.7

0.20.511.23199871.26-0.159-0.0326851.187167031.273198091.39191481.427529811.7

0.41.021.04399741.149-0.016-0.0038811.277533041.401404931.529158231.567484221.7

0.61.530.85599610.9880.0910.026924011.339789871.500692861.634671851.674865541.7

0.82.040.66799480.7480.140.053079281.299810521.482870851.61285191.651846221.7

0.92.2950.573994150.560.1380.06088941.132484041.306621851.419870251.453844771.7

0.952.42250.526993830.4150.110.052863660.914100821.058374571.149784651.177207681.7

0.9752.486250.503493660.3040.0710.035713670.700859730.806659370.876745340.897771131.7

12.550.479993500000001.7

Graficas del mtodo de Anderson para el empenaje horizontal

Calculo de coeficiente de resistencia al avance por tren de aterrizaje de narizTren de aterrizaje de nariz

ElementoNo ElementosObservacionesSuperficieCd del elementoCddel elemento referido a la superficie alar

11Cilindro0.0841.10.003683623

21Cilindro0.02241.10.000982299

32llanta0.0680.90.004879605

0.009545527

Calculo de coeficiente de resistencia al avance por tren de aterrizaje principalTren de aterrizaje principal

ElementoNo ElementosObservacionesSuperficieCd del elementoCddel elemento referido a la superficie alar

12Cilindro0.09591.10.008410939

22Cilindro0.02241.10.001964599

32llanta0.1020.90.007319407

0.017694945

Coeficiente de resistencia al avance del tren de aterrizaje totalCD' TA=0.02724047

14