1 40 AEROPLANE PERFORMANCE CALCULATIONS 



on glide found on page 116, according to the type of landing 

 used. 



K has the same value as for landing on a deck 



K 14-95^ 



= w v w 2 



Then the length run in feet to pull up on landing in still 

 air is 



1-151 , / KV,,, 2 



a 



but if a happens to be zero we must use instead for the length 

 of landing run in feet 



29V 



Examples. For numerical examples illustrating the methods 

 of this chapter, see Chapter XX., page 176. 



Theory. For theoretical explanations see Chapter VI., page 

 61. 



