曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
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┃)2/ ┃ ┃ 8 I ┃
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┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃Ac/4 ┃ ┃
┃.(')-. = 0.4 ┃ ┃ ┃ ┃ ┃ ┃t ┃deg) ┃ ┃
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┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃o ┃ ┃
┃ ┃ ┃ ┃ ┣━╋━╋━╋━┫ ┃ ┃
┃ ┃/ ┃~- ┃----- ┃ ┃ ┃ ┃ ┃ ┃ ┃
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┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃40 ┃ ┃
┃ ┃ ┃ ┣━━━╋━╋━╋━╋━┫ ┃ ┃
┃ ┃V7 ┃--- ┃ ┃ ┃ ┃ ┃ ┃50 ┃ ┃
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┃ ┃f(r ┃~ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃
┃ ┃r ┃ ┃ ┃ ┃ ┃ ┃ ┃60 ┃ ┃
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┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃ ┃
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NOTE: x is the distance from the c.g. to the a.c., positiye for the a.c. aft of the c.g,
c is the wing mean acrodynamic chord.
Fig.4 29b The parameter (CwlCDO)W for subsoruc speeds.7
PERFORMANCE, STABILITY, DYNAMICS, AND CONTROL
2zrt
b
- M=0.2
- - -. M-0,8
taper raUo=0.5
2bL
b
Flg.4.30 The parameter trpd at subsonic and supersmuc speeds]
0 < A < 3/5 deg. For other configurations not covered here, the reader may refer
to Datcom.
Estimation of qB and Cnp. The major contribution comes from vertical tail
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动力机械和机身手册2(137)