Aircraft Design - Systhesis anh Analysis 2008 Part 7 pps
Aircraft Design - Systhesis anh Analysis 2008 Part 7 pps
... for aircraft which are constrained by ground angle limits. Typical results are shown in figure 5 from data on a DC- 9-3 0, a configuration very similar to the Boeing 71 7. Laminar Airfoil Design Laminar ... Wing Geometry Definitions ● Wing Design Parameters Figure 2. The triple-slotted flap system used on a 73 7. Figure 3 shows a double-slotted flap and slat system (a 4-element ai...
Ngày tải lên: 10/08/2014, 20:20
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-...
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Aircraft Design - Systhesis anh Analysis 2008 Part 14 ppsx
... 72 .1 1949 72 .0 71 .2 71 .4 71 .5 71 .4 71 .5 71 .0 71 .2 71 .5 71 .1 71 .2 70 .8 71 .4 1950 70 .5 70 .3 70 .6 70 .7 71.0 71 .4 72 .1 72 .7 73.2 73 .6 73 .9 74 .9 72 .1 1951 76 .1 77 .0 77 .3 77 .4 77 .7 77. 6 77 .7 77 .7 78.2 78 .6 ... $) 71 7- 2 00 31.5 - 35.5 73 7- 3 00 40.0 - 46.5 73 7- 4 00 44.0 - 51.5 73 7- 5 00 34.5 - 41.0...
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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