Aircraft Design - Systhesis anh Analysis 2008 Part 7 pps

Aircraft Design - Systhesis anh Analysis 2008 Part 8 ppsx

... aviation aircraft or commuters with gear attached to turbo-prop nacelles, the value is usually much larger. Airplane ytrack / fuse dia. (approx) 73 7- 2 00 1.39 74 7- 2 00 1. 67 75 7- 2 00 1.85 76 7- 3 00 1. 67 E-3 ... aircraft or cargo aircraft that must operate without jet-ways. High wing designs may also be appropriate for STOL aircraft that make use of favorable engine-...

Ngày tải lên: 10/08/2014, 20:20

Aircraft Design - Systhesis anh Analysis 2008 Part 15 ppsx

... energy J 0 .73 756 0 1 1 0 0 Joule 0 .73 756 0 1 1 0 0 cal 3.0880 0 1 1 0 0 BTU 77 8. 17 0 1 1 0 0 erg 0 .73 756 -7 1 1 0 0 kWh 2656000 0 1 1 0 0 ! power W 0 .73 756 0 1 1 -1 0 watt 0 .73 756 0 1 1 -1 0 kW 73 7.56 ... 1996, Part 5 - Propulsion I, November 1996, Part 6 - Propulsion II, January 19 97, Part 7 - Structures, March 19 97, Part 8 - Avionics I, M...

Ngày tải lên: 10/08/2014, 20:20