Aeronautical Engineer Data Book Episode 8 pps

... 112.3 3 38. 9 182 .4 Span (m) 33.91 33.91 58 58 61.2 28. 4 34.3 20.52 20.04 28. 08 28. 08 55.57 32 .87 51.77 40.3 MAC (m) 4.29 4.29 7.26 7.26 8. 35 3 .88 4.17 3.15 3.13 3 .8 3 .8 8.04 4. 08 7. 68 5.4 Aspect ... 9.26 8. 56 8. 68 9.44 7.72 7 .85 8. 43 8. 43 7 .89 9.62 7.91 8. 9 Taper ratio 0.24 0.24 0.251 0.251 0.22 0.196 0.2 78 0. 288 0.231 0.235 0.235 0.279 0.195 0.239 0.2...

Ngày tải lên: 13/08/2014, 15:21

... 0.4025 0 .84 31 2.0947 305 .8 86 86 285 00 –41.3 0.31 78 0.3953 0 .84 02 2.1256 305.1 88 39 29000 –42.3 0.3107 0. 388 1 0 .83 72 2.1571 304.5 89 91 29500 –43.2 0.30 38 0. 381 1 0 .83 42 2. 189 2 303 .8 9144 30000 ... 0.9 289 0. 986 6 1.0622 337.4 914 3000 9.3 0 .89 62 0.9151 0. 983 9 1.0752 336 .8 1066 3500 8. 3 0 .87 98 0.9015 0. 981 2 1. 088 4 336.2 1219 4000 7.3 0 .86 37 0 .8...

Ngày tải lên: 13/08/2014, 15:21

... 000 35 000 36 089 Mach number 0 .8 0 .8 0 .83 0 .8 0 .8 0 .8 0 .8 0 .8 0 .83 0 .82 0 .8 0 .85 0.75 Thrust (lb) 1310 5 185 5725 11500 2550 1 181 3 3307 Thrust lapse rate 0.2 0.174 0.162 0. 184 0.195 0.196 ... 1996 1995 1993 1994 1 986 1 987 1993 1994 1995 1 988 1 989 1996 Thrust (lb) 7000 59 18 31 200 9220 67 500 90 000 22 000 33 000 52 200 56 750 68 000 84 000 71 100 13 85 0 6...

Ngày tải lên: 13/08/2014, 15:21

... India 11 900 18 2239N 88 27E Delhi Delhi Intl India 12 500 744 283 4N 7707E Bali Bali Intl Indonesia 984 3 14 084 5S 11510E Jakarta Intl Soerkarno-Hatta Intl Indonesia 12 0 08 34 0608S 10639E Tehran ... Malpensa Malpensa Italy 12 84 4 767 4538N 084 3E Naples Naples Italy 86 61 296 4053N 1417E Pisa Pisa Italy 980 0 9 4341N 1024E 209 202 Aeronautical Engineer s Data Book Ta...

Ngày tải lên: 13/08/2014, 15:21

... 240 Aeronautical Engineer s Data Book 13.4 Aircraft sizing/multidisciplinary design C. Bil, ‘ADAS: A Design System for Aircraft Configuration Development’, AIAA Paper No. 89 -2131. July 1 989 . ... and Development’, Institution of Mechanical Engineers (UK), proceedings, part G1, Journal of Aerospace Engineering, Vol. 203, 1 989 . 13.9 Aircraft operations Aircraft Data for P...

Ngày tải lên: 13/08/2014, 15:21

Ngày tải lên: 13/08/2014, 15:21

... Publication Data Matthews, Clifford Aeronautical engineer s data book 1. Aerospace engineering–Handbooks, manuals, etc. I. Title 629.1’3 Library of Congress Cataloguing in Publication Data Matthews, ... Stability 114 8 Principles of Propulsion 115 8. 1 Propellers 115 8. 3 Engine data lists 126 8. 4 Aero engine terminology 126 8. 5 Power ratings 129 9 Aircraft Perform...

Ngày tải lên: 13/08/2014, 15:21

... 0.35937 9.1 281 2 55/64 0 .85 937 21 .82 812 3 /8 0.37500 9.52500 7 /8 0 .87 500 22.22500 25/64 0.39062 9.92 187 57/64 0 .89 062 22.62 187 13/32 0.40625 10.3 187 5 29/32 0.90625 23.0 187 5 27/64 0.42 187 10.71562 ... 0.5 781 2 14. 684 37 3/32 0.09375 2. 381 25 19/32 0.59375 15. 081 25 7/64 0.10937 2.7 781 2 39/64 0.60937 15.4 781 2 1 /8 0.12500 3.17500 5 /8 0.62500 15 .87 500 9/64...

Ngày tải lên: 13/08/2014, 15:21

... 1 80 0 49.9 0 .8 JP 3 775 48. 4 0.775 JP 4 785 49 0. 785 JP 5 81 7 51 0 .81 7 Kerosine 82 0 51.2 0 .82 Alcohol 80 1 50 0 .80 1 Gasoline (petrol) Benzine 720 89 9 44.9 56.12 0.72 0 .89 9 Oil 89 0 ... 1.97702 0.12341 Carbon monoxide 1.25052 0.0 780 6 Helium 0.1 784 6 0.01114 Hydrogen 0. 089 88 0.005611 Nitrogen 1.250 68 0.0 780 7 Oxygen 1.42917 0. 089 212 All values...

Ngày tải lên: 13/08/2014, 15:21

... 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 ... ᎏ ␳ ∂v ᎏ ∂t + u ∂v ᎏ ∂x + v ∂v ᎏ ∂t = 1 ᎏ ␳ Y – ∂p ᎏ ∂y ᎏ ␳    78 Aeronautical Engineer s Data Book Also: K = ␳ ∆p ᎏ ∆ ␳ = ␳ dp ᎏ d ␳ and a =   =...

Ngày tải lên: 13/08/2014, 15:21