Aeronautical Engineer Data Book Episode 5 doc
Aeronautical Engineer Data Book Episode 5 doc
... flow
v
u
max
u
The flow is steady, relative
to the axes of the body
Fig. 5. 8 Flow regimes
86 Aeronautical Engineer s Data Book
5. 2.4 Sources and sinks
A source is an arrangement where a volume of ... constant
O
BA
y
x
φ = constant
of source and sink
Fig. 5. 7 Sources, sinks and combination
74 Aeronautical Engineer s Data Book
Table 4.4 Continued
NAV/COM
NDH
NOTA...
Aeronautical Engineer Data Book Episode 2 doc
... 0.218 75 5 .55 6 25 23/32 0.718 75 18. 256 25
15/ 64 0.23437 5. 953 12 47/64 0.73437 18. 653 12
1/4 0. 250 00 6. 350 00 3/4 0. 750 00 19. 050 00
17/64 0.2 656 2 6.74687 49/64 0.7 656 2 19.44687
9/32 0.281 25 7.143 75 25/ 32 ... 16.27187
5/ 32 0. 156 25 3.968 75 21/32 0. 656 25 16.668 75
11/64 0.17187 4.3 656 2 43/64 0.67187 17.0 656 2
3/16 0.18 750 4.76 250 11/16 0.68 750 1...
Aeronautical Engineer Data Book Episode 6 doc
...
Characteristics for an asymmetrical ‘infinite-span 2D airfoil’
75
50
25
0
– 25
1 .5
1.0
0 .5
0
–0 .5
5
20˚ 15
10
C
D
10 5
α
L/D
L/D
C
L
C
L
and 10
C
D
C
L
= 0 at the no-lift ... layout
ᎏ
94 Aeronautical Engineer s Data Book
y
x
z
R
r
q
R
q
θ
q
ϕ
θ
ϕ
ᎏ
∂
Fig. 5. 12 Spherical co-ordinates for axisymmetric flows
ᎏ
∂R
into a fluid flow....
Aeronautical Engineer Data Book Episode 1 potx
...
Matthews, Clifford.
Aeronautical engineer s data book / Clifford Matthews.
p. cm.
Includes index.
ISBN 0 750 6 51 25 3
1. Aeronautics–Handbooks, Manuals, etc. I. Title.
TL570.M34 2001
629.13'002'12–dc21 ... Publication Data
Matthews, Clifford
Aeronautical engineer s data book
1. Aerospace engineering–Handbooks, manuals, etc.
I. Title
629.1’3
Library of C...
Aeronautical Engineer Data Book Episode 3 ppt
... 1000 62.43 1
Sea water 10 25 63.99 1.0 25
Jet fuel JP 1 800 49.9 0.8
JP 3 7 75 48.4 0.7 75
JP 4 7 85 49 0.7 85
JP 5 817 51 0.817
Kerosine 820 51 .2 0.82
Alcohol 801 50 0.801
Gasoline (petrol) ...
Air pressure at sea level (p
0
)
6.6260 755 ϫ 10
–34
J s
8.31 451 0 J/mol/K
5. 67 051 ϫ 10
–8
W/m
2
K
4
9.806 65 m/s
2
(32.174 05 ft/s
2
)
–273.16°C (– 459 .688°F)
22....
Aeronautical Engineer Data Book Episode 4 ppsx
... 321.0
50 29 1 650 0 –17 .5 0 .53 11 0 .59 90 0.9094 1 .51 83 320.4
51 81 17000 –18 .5 0 .52 03 0 .58 92 0.9066 1 .53 88 319.8
53 34 1 750 0 –19 .5 0 .50 98 0 .57 95 0.9038 1 .55 96 319.2
54 86 18000 –20 .5 0.4994 0 .56 99 ... 0.9009 1 .58 09 318 .5
59
155 44 51 000 56 .3 0.1091 0.1 451 0.7947 5. 4773 2 95. 1
158 49 52 000 56 .3 0.1040 0.1383 0.7947 5. 7470 2 95. 1
16 154...
Aeronautical Engineer Data Book Episode 7 pps
... 1926 3037 738 848 17 05 17 05 1934 255 0 1978 410 16 05
SFC (lb/hr/lb) 0.406 0.369 0.32 0. 35 0.33 0.34 0.37 0. 351 0. 359 0.43 0 .56 3
Climb
Max thrust (lb) 758 0 18 000 55 50 62 25 15 386 3400 12 726
Flat ... 4.869 3.912 2 .59 3.1 75
Fan diameter (m) 1.272 1.219 1.9 45 1.2 45 2.794 3.404 1.681 1.681 2.477 2.477 2 .53 5 2.8 45 2.474 1 .52 2.192 1.373
Basic eng. 13 85 13 25...
Aeronautical Engineer Data Book Episode 8 pps
...
Zero-fuel 60 50 0 71 50 0 1 65 142 178 000 222 000 43 54 5 61 680 19 958 17 100 31 9 75 35 830 190 423 58 9 65 1 95 043 84 200
Max. payload 19 190 22 780 36 400 48 150 51 6 35 12 220 14 690 62 95 551 5 9302 ... 108 58 000 17 350 55 56 6 25 200
Max. fuel payload 13 50 0 19 060 – 33 160 31 450 8921 15 921 3006 3498 6 355 78 05 17 290 13 659 30 343 18 999
Design payload 14...
Aeronautical Engineer Data Book Episode 9 pdf
... 21.72 96 .5 33 85. 5 44.6
Span (m) 12. 45 12. 45 12. 45 19.06 21 .5 10.8 13.4 6. 35 7.6 10.04 10.04 20 .57 12.24 18.03 15. 1
Aspect ratio 5 5 5 4.98 4.97 4.82 5. 54 4.27 5. 16 4.64 4.64 4.38 4 .54 3.8 5. 11 ... 0.0483 0. 054 3
Seats ϫ range 4 05 000 50 2 200 1 866 410 2 3 95 250 2 9 75 000 1 45 750 463 52 0 75 600 138 030 2 0 75 3 25 348 0 75 2 192 201
(seats.nm)...
Aeronautical Engineer Data Book Episode 10 pot
...
(249 ,55 0 KG)
55
750
50 0,000 LB
(226, 850 KG)
50
PSI PSI
700
450 ,000 LB
(204, 150 KG)
400,000 LB
650
45
40
35
60
55
50
(181, 450 KG)
350 ,000 LB
600
( 150 ,800 KG)
55 0
50 0
900
850
800 ...
67.6
157
47.8
187
57 .1
202
61.7
142
43.4
171
52 .2
187
56 .9
132
40.2
159
48 .5
174
52 .9
124
37.7
150
45. 6
162
49 .5
118
35. 8
142...
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