Page 164 - Aeronautical Engineer Data Book
P. 164
Jet aircraft
r = V/f j D
e = 1/f j D
dm m 0 m 0 Vd V � L C m m d = � D R = � � m g C D f j m 1 f j m 1 g m m 0 f � L m 0 d d m C 1
C � L � C D C � L � C D
m 0 = � f m 1 m 0 fV m 1
Propeller aircraft r = /fD e = /fDV m 0 d m R = � D f m 1 m 0 dm = � E = � V fD m 1
Table 9.2 Range and endurance equations Specific range (r) Specific endurance (e) Range (R) Endurance (E)
