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...

Ngày tải lên: 13/08/2014, 15:21

... 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...

Ngày tải lên: 13/08/2014, 15:21

... 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....

Ngày tải lên: 13/08/2014, 15:21

... 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...

Ngày tải lên: 13/08/2014, 15:21

... 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....

Ngày tải lên: 13/08/2014, 15:21

... 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...

Ngày tải lên: 13/08/2014, 15:21

... 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...

Ngày tải lên: 13/08/2014, 15:21

... 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...

Ngày tải lên: 13/08/2014, 15:21

... 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)...

Ngày tải lên: 13/08/2014, 15:21

... (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...

Ngày tải lên: 13/08/2014, 15:21