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## Formulas aero

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### Informations

Catégorie :Category: mViewer GX Creator Lua TI-Nspire
Auteur Author: sauh07
Type : Classeur 3.6
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Mis en ligne Uploaded: 14/02/2020 - 23:25:38
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### Description

Conversiones de presión International Standard Atmosphere
101,325 Pa
1.01325 bar
1,013.25 mbar
1 atm
2116.2 lb/ft2
760 mmHg (torr)
29.92 inHg
33.9 ftH2O
14.696 psi
Conversiones de distancia
1 m = 3.28084 ft
1 ft = 12 in
1 mi = 1,609.34 m
1 mi = 5280 ft
1 yd = 3 ft
1 nm = 1.852 km
1 nm = 1.15078 mi
1 m/s = 3.28084 ft/s
1 km/hr = 0.277778 m/s
1 mi/hr = 1.60934 km/hr ????
1 knot [kt] = 1 nm/hr ℎ = ????+ℎ (ℎ???? )
????
1 knot [kt] = 0.51444444 m/s hG (Geométrica), h (Geopotencial)
Conversiones de temperatura Sea Level
°R = °F + 459.67
P = 101,325 Pa
K = °C + 273.15
°C = (°F -32) * (5/9)
ρ = 1.225 kg/m3
°F = (°C*(9/5)) +32 T = 288.16 K

1 kg/m3 = 0.001 kg/L ???? = ????1 + ????(ℎ − ℎ1 )
????
1 L = 1000 mL [ 0 ]
???? − ???????? +1
1 mL = 1 cm3 ????= ????1 (???? )
1
1 slug/ft3 = 515.379 kg/m3 −????0
???? ????????
???? = ????1 (???? )
Conversiones de potencia 1

1 HP = 550 ft-lb/s Isotermal
1 HP = 33,000 ft-lb/min
???? = ????1
1 HP = 745.69987158 W −????0
1 kW = 1.34102 HP ???? = ????1 ???? ???????? (ℎ−ℎ1 )
−????0
( ℎ−ℎ1 )
Otros ???? = ????1 ???? ????????
1 lbf = 4.448 N Sutherland
9.80665 N = 1 Kgf
???? 1.5 ????0 +110.4
1 Slug = 14.5939 Kg ???? = ????0 ( ) ( )
????0 ????+110.4
g0 = 9.80665 m/s2 = 32.174 ft/s2 ????????
R = 287.05 J/kg K = 1716 ft lb/slug °R ????0 = 1. 716????10−5
????????
R⨁ = 6,378,100 m ????0 = 273.15 ????
Hecho por Ariana Mi ra y Ever Renderos / Rev. Ing. Alfredo Morales
Otras Flujo Turbulento Viscoso
????∞
????= 0.37????
????∗ ????=
????????0.2
???? ∗ = √????????????
0.592
????∞????∞???? ̅ ???????????? =
???????? = ????????????0.2
????∞
1
????∞ = ????∞ ????∞ 2 ???????? =
0.074
2 ???????????? 0.2
Lift y Drag
Diseño
???? = ???????? ????∞ ????
????2
???? = ???????? ????∞ ???? ???????? =
???? ????
???????????????????? ???????????????????? = tan−1 ???? ????????????????
????=
???????? 2 ????????????????????
????????,???? =
???????????????? 2????????????????????(1+????+????2)
????̅ =
???????? = ???????? + ????????,???? 3 ( 1+????)
???? 2 ???????????????????? =
2????
???????? = ???????? + ???? ???? ( 1+????)
????????????????
???????? = ????(???? − ????????=0 )
Distribución de Presiones y Esfuerzos cortantes
???????????? ????0
????= = 180(???? )
???????? 1+ 2 0 ????????
????´ = − ∫???????? (???????? ???????????????? + ???????? ????????????????)???????????? +
???? ????1 ????????
????????2 −????????1 ????????
????0 = ∫???????? (???????? ???????????????? − ???????? ????????????????)????????????
????2 −????1
????????
Flujo incompresible M<0.3 ????´ = ∫???????? (−???????? ???????????????? + ???????? ????????????????)???????????? +
????????
???????? = ???????? + ????∞ ∫???????? (???????? ???????????????? + ???????? ????????????????)????????????
Flujo compresible 0.3<M<1
????
????0 ????−1 ????−1
= (1 + ????2 )
????1 2
1
????0 ????−1 ????−1
= (1 + ????2 )
????1 2
????0 ????−1
= 1+ ????2
????1 2

*1-Estático, 0-Stagnation
Flujo Supersónico
????
????02 ( ????+1) 2????2 ????−1 1−????+2???????? 2
=[ ] ∗
????1 4???????? 2−2( ????−1 ) ???? +1

Flujo Laminar Viscoso ???? = ???? cos ???? − ???? sin ????
5.2????
????= ???? = ???? sin ???? + ???? cos ????
√????????????
0.664???? ∞
???????? =
√????????????
0.664
???????????? =
√????????????
1.328
???????? =
√????????????

Hecho por Ariana Mi ra y Ever Renderos / Rev. Ing. Alfredo Morales

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