- Intro/History
- Stock Research --> sr 01
- CompMatPertrb --> cm 01
- CompMatPertrb-->>cm 02
- CompMatPertrb --> cm 03
- Inter. pipe/soil--> ps 01
- Flt Fuel Eff --> fm 01
- Flt Fuel Eff--> fm 02
- Flt Fuel Eff--> fm 03
- Flt Fuel Eff--> fm 04
- Flt Fuel Eff--> fm 05
- Flt Fuel Eff--> fm 06
- Technical Note 10162023
- Flt Fuel Eff --> fm 07
- Flt Fuel Eff --> fm 08
- CircArc 1--> nq 01
- CircArc 2--> nq 02
- CircArc 3--> nq 03
Math Theory of Flight Fuel Efficiency --> fm 01
Application Example: Ascending with several path angles
Application Example: Ascending with several initial speeds
Application Example: Ascending with several initial speeds
The airplane is a typical commercial jetliner of total weight 475000 pounds including a fuel capacity of 44953 pounds, ascending with an initial speed of 278 ft/s at see level, and path angles of 5, 10, 20, and 25 degrees., respectively.
Application Example: Ascending with several initial speeds
Application Example: Ascending with several initial speeds
Application Example: Ascending with several initial speeds
The airplane is a typical commercial jetliner of total weight 475000 pounds including a fuel capacity of 44953 pounds, ascending with initial speed of 278 ft/s, 288 ft/s, 298 ft/s at see level, respectively, and a path angle of 5 degrees.
