Aircraft Design: Synthesis and Analysis - part 10 doc
Aircraft Design: Synthesis and Analysis - part 10 doc
... 99.4 99.7 100 .2 100 .5 100 .7 101 .0 101 .3 101 .6 100 .0 1968 102 .0 102 .3 102 .8 103 .1 103 .4 104 .0 104 .5 104 .8 105 .1 105 .7 106 .1 106 .4 104 .2 1969 106 .7 107 .1 108 .0 108 .7 109 .0 109 .7 110. 2 110. 7 111.2 ... -2 0 0 bar 2.08858 3 1 -2 0 0 inHg 70.727 0 1 -2 0 0 mmHg 2.7845 0 1 -2 0 0 torr 2.7845 0 1 -2 0 0 inH2O 5.2024 0 1 -2 0 0...
Ngày tải lên: 08/08/2014, 11:21
Aircraft Design: Synthesis and Analysis - part 1 doc
... Thus the DC- 9-1 0, a 77,000 lb, 80 passenger airplane grew into a DC- 9-2 0, then the -3 0, -4 0, -5 0, -8 0 then on to the MD-80 and MD-90 series. The MD-90 weighs as much as 172,000 lbs and can carry ... first to fly. Aircraft Design: Synthesis and Analysis The Airline Industry In order to understand how new aircraft might fit into the current mar...
Ngày tải lên: 08/08/2014, 11:21
Aircraft Design: Synthesis and Analysis - part 8 docx
... less than 110 percent of VMU in the all- engines-operating condition and not less than 105 percent of VMU determined at the thrust-to-weight ratio corresponding to the one-engine-inoperative ... concentrations around splices, cut-outs, doors, windows, access panels, etc., and to serve as tear-stoppers at frames and longerons. Generally DC -1 0 uses 2024-T3 aluminum for tension st...
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Aircraft Design: Synthesis and Analysis - part 2 pptx
... environment Moderate-to-long runways Paved runway High -level ATC and landing aides Adequate space for ground maneuver and parking Short-to-moderate runways All types of runway surfaces Often spartan ... (bn) Index Passengers carried (m) Index RPKs (bn) Index 1976 22 100 60 100 241 100 314 100 1977 23 104 .5 66 110. 0 259 107 .5 338 107 .6 1978 25 113.6 78 130.0 293 121.6 39...
Ngày tải lên: 08/08/2014, 11:21
Aircraft Design: Synthesis and Analysis - part 3 ppt
... component at zero-lift and a lift-dependent component but includes only the increments due to Mach number (C L and Re are assumed to be constant.) Zero-lift drag is the drag at M=0.5 and C L = 0. ... emergency exit with respect to dimensions, step-up and step-down distance, and with the top of the opening not less than 56 inches from the passenger compartment floor, 15 additiona...
Ngày tải lên: 08/08/2014, 11:21
Aircraft Design: Synthesis and Analysis - part 4 potx
... popular airfoils of the time: +- y = (t/0.2) * (.2969*x 0.5 - .126*x - .3537*x 2 + .2843*x 3 - .101 5*x 4 ) The camberline of 4-digit sections was defined as a parabola from the leading edge ... numbers for which the above analysis is not appropriate. In supersonic flow an aircraft has lift and volume-dependent wave drag in addition to the viscous friction and vort...
Ngày tải lên: 08/08/2014, 11:21
Aircraft Design: Synthesis and Analysis - part 5 pdf
... designed for efficient high-speed flight is often quite different from one designed solely for take- off and landing. Take-off and landing distances are strongly influenced by aircraft stalling speed, ... deflection of 0 deg and 20 deg. Airplane S wf / Sref Flap Type Flap Chord Ratio Sweep (deg) DC-3S 0.575 Split 0.174 10 DC-4 0.560 Single Slot 0.257 0 DC-6 0.589 Double Slot 0.2...
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Aircraft Design: Synthesis and Analysis - part 6 pot
... "good-flying" and difficult-to-fly aircraft. New aircraft designs can be simulated to determine whether they are acceptable. Such real-time, pilot-in-the- loop simulations are expensive and ... small 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-flap interacti...
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Aircraft Design: Synthesis and Analysis - part 7 pps
... 70" 1100 Aero Vodochody L-139 ALF502/507 670 0-7 800 0.4 3-0 .41 50" 65" 1350 Ch 600, Bae-146, AvroRJ Allison http://www.allison.com/ AE3007 7200 0.39 43" 106 " 1580 Citation-X, ... for which Williams/Rolls-Royce //www.rolls-royce.com/ F107/F112 700 N/A 12" 40" 146 ALCM, Tomahawk FJX-2 700 N/A 14" 41" 100 V-Jet 2 FJ4 4-1 ,2 190 0-2 300...
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Aircraft Design: Synthesis and Analysis - part 9 pot
... area and structure capable of much greater range than the DC-1 0-1 0. The overwater DC-l 0-3 0 with a range comparable to the B747 would show about the same ¢/seat-mile as the B-747. Figures 13 and ... in Fig. 11 where the $/stat-mile is plotted for very different sized aircraft. The DC -1 0 shown is the domestic version, the DC-1 0-1 0. The corresponding ¢/seat stat-mile is s...
Ngày tải lên: 08/08/2014, 11:21