Table 1: Comparison of normalized central deflections, , of antisymmetric [0/90] plates and spherical panels under uniform load for different a/h ratios.

Normalized central deflection, , of [0/90] panels under uniform load

 

a/h

 

R1 = R2

= ∞ (SS1)  [100]

R1 = R2

= ∞ (SS3)

R1 = R2

= ∞ (SS4)

[100]

R1/a = R2/a = 10 (SS1)

[101]

R1/a = R2/a = 10 (SS3)

R1/a = R2/a = 10 (SS4)

 

Comments

5

 

25.78966

 

 

25.791

(0.0052)*

25.410

(1.4721)*

 

25.62255

(0.6480)ǂ

 

25.594

(0.1114)*

(0.7624 )ǂ

 

23.237

(9.3104)*

(8.5601)ǂ

 

Some membrane action, insignificant restraint effect

10

 

19.17171

 

 

19.173

(0.0067)*

 

18.793

(1.9754)*

 

18.81966

(1.8363 )ǂ

 

18.744

(0.4020)*

(2.2326 )ǂ

 

14.881

(20.9284)*

(20.8299 )ǂ

Reasonably high membrane action,

insignificant restraint effect

 

20

 

17.50887

 

17.509

(0)*

17.138

(2.1182)*

16.44626

(6.0690 )ǂ

 

16.164

(1.7163)*

(7.6848)ǂ

8.836

(46.2735)*

(48.4629)ǂ

High membrane action, insignificant restraint effect

50

 

17.04309

17.043

(0)*

16.676

(2.1539)*

12.38411

(27.3365)ǂ

 

11.296

(8.7863)*

(33.7216)ǂ

 

2.446

(80.2489)*

(85.3421)ǂ

 

Very high membrane action, insignificant restraint effect

 

100

 

16.97656

16.977

(0)*

16.609

(2.1651)*

 

6.81361

(59.8646)ǂ

 

5.539

(18.707)*

(67.3743)ǂ

0.651

(90.4456)*

(96.0848)ǂ

Very high membrane action, insignificant restraint effect

%Difference Edge Restraint = SSx-SS1 SS1 100,x=3,4

%Difference Curvature = Shel l x Plat e x Plat e x 100,x=1,3,4.