The Breguet range equation was developed for cruise climb flight of a jet aircraft to include the climb angle and is then maximized with respect to the no wind true airspeed. The expression for the best range airspeed is a function of the specific fuel consumption and minimum drag airspeed and indicates that an operational airspeed equal to the fourth root of three times the minimum-drag airspeed introduces range penalties of the order of one percent.
Best-range flight conditions for cruise-climb flight of a jet aircraft
1976-01-01
Conference paper
No indication
English
British Library Conference Proceedings | 2015
|Cruise Range in Formation Flight
AIAA | 2017
|Cruise Range in Formation Flight
Online Contents | 2017
|