DEFLECTIONS OF AN INFLATED CIRCULAR-CYLINDRICAL CANTILEVER BEAM

被引:127
作者
COMER, RL
LEVY, S
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关键词
D O I
10.2514/3.1873
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
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页码:1652 / 1655
页数:4
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共 10 条
[1]   STABILITY OF A CONSOLE CYLINDRICAL SHELL UNDER BENDING BY A TRANSVERSE FORCE WITH TWISTING AND INTERNAL PRESSURE [J].
DAREVSKII, VM .
ARS JOURNAL, 1961, 31 (01) :125-133
[2]  
FUNG VC, 1957, J AERONAUT SCI, V24, P351
[3]  
HARRIS JT, 1961, ASTRONAUTICS, V6, P30
[4]   THE STABILITY OF THIN-WALLED UNSTIFFENED CIRCULAR CYLINDERS UNDER AXIAL COMPRESSION INCLUDING THE EFFECTS OF INTERNAL PRESSURE [J].
HARRIS, LA ;
SUER, HS ;
SKENE, WT ;
BENJAMIN, RJ .
JOURNAL OF THE AERONAUTICAL SCIENCES, 1957, 24 (08) :587-596
[5]  
HOPKINS HG, 1951, AMES RES CTR REPT ME, V2423
[6]  
LEONARD RW, 1960, NASA TN D457
[7]  
LO H, 1951, NACA TN1027
[8]  
PETERSON JP, 1960, NASA TN D526
[9]  
STEIN M, 1961, NASA TN D813
[10]  
TOPPING AD, 1954, GER5850 GOOD AIRCR C