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...
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...
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...
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...
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...
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...
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...
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...
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...
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...
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