Calculating landing distance for Flight

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Homework Statement


An a/c has an approach speed of45 m/s with descent angle of 7.1 deg. if the a/c load factor is 1.2 and constant deceleration at touch down is .25g (g=9.81).its total landing distance approx over a 15m high obstacle is

Homework Equations



R=v/g(n-1)
Sa=(h-hf)/tan( teta)
Sf=Rsin(teta)
hf=R(1-cos(teta)
Sg=v2m/(2*F)
R-radius,hf-flare height,Sa-approach dist,Sf-flare distance,Sg-ground roll
S=Sa+Sf+Sg

The Attempt at a Solution


well i have found value for approach and flare distance.but for ground roll I am lacking mass to consider for calculation or do i miss smeting?.. any suggestion wld be helpfull.[/B]
 
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praveenpandiyan said:

Homework Statement


An a/c has an approach speed of45 m/s with descent angle of 7.1 deg. if the a/c load factor is 1.2 and constant deceleration at touch down is .25g (g=9.81).its total landing distance approx over a 15m high obstacle is

Homework Equations



R=v/g(n-1)
Sa=(h-hf)/tan( teta)
Sf=Rsin(teta)
hf=R(1-cos(teta)
Sg=v2m/(2*F)
R-radius,hf-flare height,Sa-approach dist,Sf-flare distance,Sg-ground roll
S=Sa+Sf+Sg

The Attempt at a Solution


well i have found value for approach and flare distance.but for ground roll I am lacking mass to consider for calculation or do i miss smeting?.. any suggestion wld be helpfull.[/B]
in your work-energy equation for Sg, m/F per Newton 2 is given! Or use the kinematic equations instead.
 
You have an initial horizontal velocity at touchdown and the deceleration. That's enough. For ground roll, and leaving aside air resistance, mass doesn't matter.
 
yeah.i see it now,its a simple force eqn. thanks all