Aeronautical Engineer Data Book Episode 10 pot

... parking bays and manoeuvring 176 Aeronautical Engineer s Data Book Fig. 11.2 Birmingham airport – a crossed runway layout 178 Aeronautical Engineer s Data Book Aircraft design Ground manoeuvring ... 1.04 E (GE) 2 -10 0.85 3-1 0.93 E (RR) 3-7 1.09 3 -10 1.17 F 16 -10 5.14 17-4 5.28 G (Large door) 10- 7 3.23 11-2 3.41 G (Small door) 10- 6 3.22 11-...

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, ... 10 Aeronautical Engineer s Data Book Table 2.4 Density (␳) Unit lb/in 3 lb/ft 3 kg/m 3 g/cm 3 1 lb per in 3 1 1728 2.768 27.68 ϫ 10 4 1 lb per ft 3 5.787...

Ngày tải lên: 13/08/2014, 15:21

... important when there is a mating hole-to-shaft fit. 230 Aeronautical Engineer s Data Book CAE CAD CAM 100 1100 10 100 1 0100 1 0101 0101 0 Central CAD/CAM computer facility Analysis and modelling ... preferred sizes Fig. 12.2 The R5 and R10 series 220 -0.00 Aeronautical Engineer s Data Book ? 10 +0.05 10 +0.05 10 +0.05 10 nominal 10 +0.05 10 +1.0...

Ngày tải lên: 13/08/2014, 15:21

... dm 2 15.5 0 .107 6 0.01196 – 100 1 0.01 – – – 1 m 2 1550 10. 76 1.196 – 10 000 100 1 0.01 – – 1 are (a) – 107 6 119.6 – – 10 000 100 1 0.01 – 1 hectare (ha) – – – – – – 10 000 100 1 0.01 1 ... 2.778 ϫ 10 –4 0.2161 3.929 ϫ 10 –4 7.000 ϫ 10 –2 2.930 ϫ 10 –4 0.2930 1 BTU/s 3600 1 777.9 1.414 252.0 1.055 1.055 ϫ 10 –3 1ft-lb/s 4.62 1.286 ϫ 10 –3 1 1.818 ϫ 10...

Ngày tải lên: 13/08/2014, 15:21

... ᎏᎏ + v ᎏᎏ dx dx dx d u 1 du u dv ᎏᎏ ᎏᎏ = ᎏᎏ ᎏᎏ – ᎏᎏ ᎏᎏ dx v v dx v 2 dx  44 Aeronautical Engineer s Data Book Circle General equation x 2 – y 2 + 2gx + 2fy + c = 0 The centre has co-ordinates ... equation of a hyperbola is ᎏᎏ – ᎏᎏ = 1 2 a b 2 where b 2 = a 2 (e 2 – 1). 48 Aeronautical Engineer s Data Book 3. Federal Standard 376B: 1993: Preferred Metric Unit...

Ngày tải lên: 13/08/2014, 15:21

... 299.9 100 58 33000 –50.2 0.2586 0.3345 0.8134 2.4318 299.2 102 10 33500 –51.2 0.2526 0.3282 0. 8104 2.4692 298.6 103 63 34000 –52.2 0.2467 0.3220 0.8073 2.5074 297.9 105 15 34500 –53.2 0.2 410 0.3159 ... 0.7947 12.399 295.1 2103 1 69000 –56.3 0.4593 –1 0. 6108 –1 0.7947 13. 010 295.1 21336 70000 –56.3 0.4377 –1 0.5822 –1 0.7947 13.650 295.1 63 68 Aeronautical Engineer s D...

Ngày tải lên: 13/08/2014, 15:21

... (UK) Military engineering division airfield (UK) Minimum descent height Special rules airspace (area) Special rules zone Terminal control area 72 Aeronautical Engineer s Data Book Table 4.3 ... 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 NOTAM O/H OAT OC OMEGA...

Ngày tải lên: 13/08/2014, 15:21

... + 1 5.8 Axisymmetric flows Axisymmetric potential flows occur when bodies such as cones and spheres are aligned 100 Aeronautical Engineer s Data Book Arrow length represents the magnitude ... linear quanti- ties in matrix format:  = D  Ox 0 Oy 0 Oz 0 Ox 3 Oy 3 Oz 3 108 Aeronautical Engineer s Data Book x b x w z b z w y b, .y w V 0 Conventional body axis system. O x...

Ngày tải lên: 13/08/2014, 15:21

... Very stable Fig. 7.6 Degree of stability (static, longitudinal) 120 Aeronautical Engineer s Data Book Engine efficiency (%) 100 90 Turboprop 80 70 Turbofan 60 Turbojet 50 0.5 0.6 0.7 ... 0.82 0.8 0.85 0.75 Thrust (lb) 1 310 5185 5725 11500 2550 11813 3307 Thrust lapse rate 0.2 0.174 0.162 0.184 0.195 0.196 Flat rating (°C) ISA +10 ISA +10 ISA +10 ISA +10 SFC (lb/h...

Ngày tải lên: 13/08/2014, 15:21

... and the braked roll to a standstill. 146 Aeronautical Engineer s Data Book L ow w i ng Hi g h w i ng Straight-wing turboprop High-wing turbofan AR =10. 5 AR=8.9 Twin engine Airbus AR=9.4 ... /Doug. /Doug. Tu-204 Model 200 200 200 300 500 200 800 100 ER EMB-145 F70 F100 II-96M MD-90-30 MD-11 -200 Average t/c % 11.6 10. 83 11 10. 28 10. 28 11 9.35 1/4 chord sweep (°) 25...

Ngày tải lên: 13/08/2014, 15:21