- 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 02
Application Example: Descending Actions:
The same commercial jetliner descends from an altitude of 32000 feet with a speed of 443 MPH and a 10% fuel capacity. Path angles: -4 to -7 degrees.
Application Example: Descending Actions
The same commercial jetliner at 7016 feet with a preset speed of 172.5 MPH and a 10% fuel capacity. Path angles: -1 to -4 degrees. Interesting note: near-perfect linearities.