Расчет на прочность крыла большого удлинения и шасси транспортного самолета АН–70

148 РЕДУЦИР. ТОЛЩИНЫ

OБЩИE ДAHHЫE M XI YI FI .0040

7200E+11 29 .0000 .0000 .1000E-14 .0060

-.5500E+09 4 1.0290 .4970 .1387E-01 .0060

-.3440E+09 3 1.2540 .5210 .2780E-02 .0060

1201E+08 4 1.5570 .5390 .2780E-02 .0060

1290E+07 2 1.8600 .5760 .2780E-02 .0060

0000E+00 29 2.1620 .5450 .2780E-02 .0060

1190E+07 15 2.4650 .5380 .2780E-02 .0060

-.3403E+05 16 2.7670 .52

50 .2780E-02 .0060

2145E+01 3.0700 .5080 .2780E-02 .0060

3.3710 .4860 .2780E-02 .0060

3.6730 .4600 .2780E-02 .0060

3.9750 .4310 .2780E-02 .0060

4.2730 .3990 .2780E-02 .0060

4.5770 .3640 .2780E-02 .0032

4.8020 .3360 .8030E-02 .0072

4.8020 -.1660 .3770E-02 .0072

4.5760 -.1810 .2330E-02 .0072

4.2720 -.2000 .2330E-02 .0072

3.9730 -.2170 .2330E-02 .0072

3.6710 -.2320 .2330E-02 .0072

3.3670 -.2460 .2330E-02 .0072

3.0670 -.2590 .2330E-02 .0072

2.7650 -.2580 .2330E-02 .0072

2.4630 -.2680 .2330E-02 .0072

2.1610 -.2740 .2330E-02 .0072

1.8590 -.2760 .2330E-02 .0072

1.1560 -.2730 .2330E-02 .0072

1.2550 -.2650 .2330E-02 .0052

1.0290 -.2500 .7690E-02 .0080

MX= .11948E+08 MY= .17681E+07 NZ= .00000E+00 IX= .15907E-02

IY= .10304E+00 FS= .39432E-01 Итераций- 19

ПОТОКИ КАСАТЕЛЬНЫХ

HАПРЯЖEHИЯ ГЛАВНЫЕ ЦЕНTPAЛЬНЫЕ РЕДУKЦИOНHЫE УCИЛИЙ

ДEЙСTBИTEЛЬHЫE Х y КOЭФФИЦИЕНТЫ -.4989E+05

.3665E+09 -.2683E+01 -.4955E+00 .1007 -.3133E+06

-.3473E+09 -.1674E+01 .4213E-01 1.0060 -.2319E+06

-.3023E+09 -.1450E+01 .7508E-01 .5168 -.1480E+06

-.3069E+09 -.1148E+01 .1051E+00 .3820 -.6102E+05

-.3144E+09 -.8470E+00 .1542E+00 .2704 .2529E+05

-.3113E+09 -.5440E+00 .1353E+00 .3062 .1122E+06

-.3120E+09 -.2410E+00 .1403E+00 .2973 .1993E+06

-.3118E+09 .6128E-01 .1394E+00 .3006 .2866E+06

-.3109E+09 .3647E+00 .1345E+00 .3123 .3738E+06

-.3092E+09 .6664E+00 .1245E+00 .3376 .4609E+06

-.3070E+09 .9692E+00 .1105E+00 .3803 .5480E+06

-.3042E+09 .1272E+01 .9361E-01 .4500 .6354E+06

-.3010E+09 .1571E+01 .7351E-01 .5771 .7213E+06

-.2873E+09 .1876E+01 .5066E-01 .8280 .9070E+06

-.2029E+09 .2102E+01 .3165E-01 1.0060 .7280E+06

4757E+09 .2122E+01 -.4700E+00 .1347 .6424E+06

3679E+09 .1897E+01 -.4939E+00 .0992 .5556E+06

3727E+09 .1594E+01 -.5250E+00 .0947 .4677E+06

3771E+09 .1296E+01 -.5540E+00 .0910 .3786E+06

3813E+09 .9947E+00 -.5810E+00 .0878 .2886E+06

3853E+09 .6915E+00 -.6071E+00 .0850 .1976E+06

3891E+09 .3923E+00 -.6320E+00 .0826 .1061E+06

3908E+09 .9050E-01 -.6431E+00 .0816 .1376E+05

3941E+09 -.2109E+00 -.6651E+00 .0796 -.7929E+05

3968E+09 -.5124E+00 -.6831E+00 .0781 -.1729E+06

3989E+09 -.8141E+00 -.6972E+00 .0770 -.2675E+06

4026E+09 -.1517E+01 -.7222E+00 .0752 -.3617E+06

4007E+09 -.1418E+01 -.7103E+00 .0761 -.4989E+05

5140E+09 -.1644E+01 -.7043E+00 .0986 .7110E+06

Равнодействующие нормальных напряжений:

MX= .11844E+08 MY= .18281E+07 NZ=-.73329E+05

Приложение 2

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