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12
Aliran Udara
Lift Coeffisien adalah perbandingan dari tekanan gaya angkat/lift dengan tekanan dinamik yang
merupakan fungsi dari bentuk sayap dan sudut serang
. a "lift coefficient" would be the ratio between lift pressure and dynamic pressure, a "drag
coefficient" would be the ratio between drag pressure and dynamic pressure.
Dynamic pressure represents the kinetic energy of the free airstream and is a factor relating the
capability for producing changes in static pressure on a surface.
TABLE 1-1. Effect of Speed and Altitude on Dynamic Pressure
---------------------------------------------------------------------------
: : Dynamic pressure, q, psf
Velocity : True Airspeed :-----------------------------------------------
(knots) : (ft/sec) : Sea level : 10,000 : 20,000 : 30,000 : 40,000
: : : ft : ft : ft : ft
----------:----------------:-----------:--------:--------:--------:--------
: s = : 1.000 : 0.7385 : 0.5328 : 0.3741 : 0.2462
----------:----------------:-----------:--------:--------:--------:--------
100 : 169 : 33.9 : 25.0 : 18.1 : 12.7 : 8.4
200 : 338 : 135.6 : 100.2 : 72.3 : 50.7 : 33.4
300 : 507 : 305 : 225 : 163 : 114 : 75.0
400 : 676 : 542 : 400 : 289 : 203 : 133
500 : 845 : 847 : 625 : 451 : 317 : 208
600 : 1,013 : 1,221 : 902 : 651 : 457 : 300
---------------------------------------------------------------------------
q = 1/2 rV2
where
q = dynamic pressure, psf
δ = air density, slugs per cu ft
V = air velocity, ft/sec
or q = .00339sV2
where s = density ratio
V = true velocity, knots
0.00339 = constant which allows use of knots as velocity units and the altitude density ratio
an alternate form is
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  • 58. Lift Coeffisien adalah perbandingan dari tekanan gaya angkat/lift dengan tekanan dinamik yang merupakan fungsi dari bentuk sayap dan sudut serang . a "lift coefficient" would be the ratio between lift pressure and dynamic pressure, a "drag coefficient" would be the ratio between drag pressure and dynamic pressure. Dynamic pressure represents the kinetic energy of the free airstream and is a factor relating the capability for producing changes in static pressure on a surface. TABLE 1-1. Effect of Speed and Altitude on Dynamic Pressure --------------------------------------------------------------------------- : : Dynamic pressure, q, psf Velocity : True Airspeed :----------------------------------------------- (knots) : (ft/sec) : Sea level : 10,000 : 20,000 : 30,000 : 40,000 : : : ft : ft : ft : ft ----------:----------------:-----------:--------:--------:--------:-------- : s = : 1.000 : 0.7385 : 0.5328 : 0.3741 : 0.2462 ----------:----------------:-----------:--------:--------:--------:-------- 100 : 169 : 33.9 : 25.0 : 18.1 : 12.7 : 8.4 200 : 338 : 135.6 : 100.2 : 72.3 : 50.7 : 33.4 300 : 507 : 305 : 225 : 163 : 114 : 75.0 400 : 676 : 542 : 400 : 289 : 203 : 133 500 : 845 : 847 : 625 : 451 : 317 : 208 600 : 1,013 : 1,221 : 902 : 651 : 457 : 300 --------------------------------------------------------------------------- q = 1/2 rV2 where q = dynamic pressure, psf δ = air density, slugs per cu ft V = air velocity, ft/sec or q = .00339sV2 where s = density ratio V = true velocity, knots 0.00339 = constant which allows use of knots as velocity units and the altitude density ratio an alternate form is