Presentation is loading. Please wait.

Presentation is loading. Please wait.

1 Master Of Science Aerospace Engineering Proyecto Final “FRANKY”

Similar presentations


Presentation on theme: "1 Master Of Science Aerospace Engineering Proyecto Final “FRANKY”"— Presentation transcript:

1 1 Master Of Science Aerospace Engineering Proyecto Final “FRANKY”

2 2 Master of Science in Aerospace engineering PRIMER ESTIMADO DE PARAMETROS FIRST ESTIMATE AR e k T k P N/m2 Dens kg/m3 weight (W0)6.9kg Altura (h)500mts. W fin6.82kg. R -gas J/K kmol m aire28.96kg/kmol R tierra6356km g09.81m/s2 T K P N/m2 Dens kg/m3 W crew0.46kg. W Payload2.07kg. W Fuel0.08kg. Wempty6.5kg. HorsePower1.15hp n fuel E max Engine Power825lb*ft/seg V max37.27ft/seg

3 V max37.27ft/seg V max11.43m/seg. Vel. Sonido (a)336.43J/kg Mach Number (M)0.05m/s K Re Log Re^ Cf A Superior2.3mts^2 A Lateral1.8mts^2 S wet4.1mts^2 a0 para 0' (Tabla 2.6)0.11grados a0 radianes6.0Radianes a (pendiente elev.)1.2por radian a grados0.1Grados Angulo ataque4.0Grados CL C Di C D CD D L E Master Of Science Aerospace Engineering PRIMER ESTIMADO DE PARAMETROS

4 CARACTERISTICAS DEL ALA 4 Master Of Science Aerospace Engineering

5 CONFIGURACION DEL ALA 5 Master Of Science Aerospace Engineering

6 Aerospace Prototype Generation PERFIL DEL ALA selig/uiuc_lsat_airfoilsTested.html 6 Master Of Science Aerospace Engineering

7 PERFIL DEL ALA 7 Master Of Science Aerospace Engineering

8 Aerospace Prototype Generation ESTRUCTURA DEL ALA 8 Master Of Science Aerospace Engineering

9 Aerospace Prototype Generation ESTRUCTURA DEL ALA 9 Master Of Science Aerospace Engineering

10 Aerospace Prototype Generation ESTRUCTURA DEL ALA 10 Master Of Science Aerospace Engineering

11 Aerospace Prototype Generation ESTRUCTURA DEL ALA 11 Master Of Science Aerospace Engineering

12 Aerospace Prototype Generation ESTRUCTURA DEL ALA 12 Master Of Science Aerospace Engineering

13 PLANTILLAS DEL ALA 13 Master Of Science Aerospace Engineering

14 Aerospace Prototype Generation PLANTILLAS DEL ALA 14 Master Of Science Aerospace Engineering

15 CONFIGURACION DEL EMPENAJE Empenaje Convencional Tail Volume Ratios: Horizontal Tail V HT = 0.7 Vertical Tail: VvT = Master Of Science Aerospace Engineering

16 Aerospace Prototype Generation CONFIGURACION DEL EMPENAGE in in in L HT 16 Master Of Science Aerospace Engineering

17 CONFIGURACION DEL EMPENAGE 17 Master Of Science Aerospace Engineering Horizontal Tail V HT0.70 V VT0.04 IHT35.17in IVT30.59in c11.25in S HT151.14in^2 SVT63.0in^2 AR for H TAIL4.00 bt24.59in H Taper ratio λ0.50 crt8.20in ctt4.10in yHT5.46in cHT6.37in

18 Aerospace Prototype Generation MODELADO DEL ALA HORIZONTAL 18 Master Of Science Aerospace Engineering

19 Aerospace Prototype Generation MODELADO DEL ALA HORIZONTAL 19 Master Of Science Aerospace Engineering

20 Aerospace Prototype Generation EMPENAJE 20 Master Of Science Aerospace Engineering

21 Aerospace Prototype Generation ESTRUCTURA 21 Master Of Science Aerospace Engineering

22 Aerospace Prototype Generation 22 Master Of Science Aerospace Engineering EMPENAJE

23 Aerospace Prototype Generation 23 Master Of Science Aerospace Engineering EMPENAJE

24 Aerospace Prototype Generation 24 Master Of Science Aerospace Engineering EMPENAJE

25 Aerospace Prototype Generation 25 Master Of Science Aerospace Engineering EMPENAJE

26 Aerospace Prototype Generation 26 Master Of Science Aerospace Engineering EMPENAJE

27 27 Master Of Science Aerospace Engineering EMPENAJE

28 Aerospace Prototype Generation CALCULOS DE FUSELAJE 28 Master Of Science Aerospace Engineering W dataWeightUnits W motor1.22lbs W Fuel0.08lbs W S. Carburador0.024lbs W pila0.05lbs W Tx. Y Servo ala0.05lbs W Baggage2.07lbs Book-Dimentions ratio Nose/motor2.0in. Nose/Fuel6.4in. Nose/S. Carburador14.0in. Nose/Pila16.5in. Nose/Tx, S. ala19in. Nose/Baggage24in. Effective c.g. of 3 weights without wing c.g. without wingDistanceUnits x15.66in. Effective c.g. of 3 weights with wing c.g. with wingDistanceUnits x15.6in.

29 Aerospace Prototype Generation Fuselage length Wing Chord c.g. w/o wing c.g. with wing W People W Engine W Baggage 29 Master Of Science Aerospace Engineering EMPENAJE

30 CALCULOS DE FUSELAJE 30 Master Of Science Aerospace Engineering Ratio Units Nose-Ground in Nose-Wing in Nose-a.c. in Nose-c.g in b60in cr12.25in* ct12.25in* y15 c12.25in Xn16.81in (Xac)wing16.11in x12.86in Xc18.98in Nosewheel4.42in

31 CALCULOS DE FUSELAJE 31 Master Of Science Aerospace Engineering SG por requerimiento60mts Vlo37.988ft/s Sg=22.557/(t/w) R ft qob8.75grados Sa39.214ft T/W0.142a 0.7 Vlo V26.592ft/s Pr = T * V45.249ftlb/s P60.332ft lb/s P min requerida hp

32 CALCULOS DE FUSELAJE 32 Master Of Science Aerospace Engineering Units Vf45.84ft/s R326.50ft sen 3' cos 3' tan 3' Obstacle5ft j1.15° µ hf0.457ft Sa86.7ft Sf17.1ft Sg199.9ft Delta Cl max0.5 Cl max CL max T/W0.0864

33 CALCULOS DE FUSELAJE 33 Master Of Science Aerospace Engineering

34 CALCULOS DE FUSELAJE 34 Master Of Science Aerospace Engineering

35 CALCULOS DE FUSELAJE 35 Master Of Science Aerospace Engineering


Download ppt "1 Master Of Science Aerospace Engineering Proyecto Final “FRANKY”"

Similar presentations


Ads by Google