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ISOGRID-SST™ Typical Results

ISOGRID-SST™ outputs include numerous graphical and alpha numeric results. Typical inputs are geometry, clearance envelopes, material properties, knockdown factors, margins of safety, design criteria, minimum gauges and manufacturing tolerances.

Some ISOGRID-SST™ generated results are reviewed here.

Cross section properties

Elastic skin buckling, which reduces effective skin in the rib cross section, is an allowable ISOGRID-SST™ design criteria, albeit that structural performance is reduced due to the reduction in effective rib cross section properties.

In converging on a final design, ISOGRID-SST™ selectively evaluates minimum, average and maximum manufacturing tolerances. The minimum gauges (due to maximum tolerances) are not always the most critical. In some cases the maximum gages (due to minimum tolerances) attract undesirably high internal loads. ISOGRID-SST™ evaluates such conditions in developing optimum structural design definition parameters. 

ISOGRID-SST™ selects optimum design parameters by maximizing the margin floors for such failure modes as rib, skin and flange buckling. This process is repeated for all loading conditions to generate an optimum design definition.

Outputs can be in either English or SI units.

Summary of element numerical data.

The following  is an example of ISOGRID-SST™ alpha numeric results.

Applicable margins are summarized at the bottom of the chart.

ISOGRID-SST™ also produces such results for un-flanged isogrid, flanged and un-flanged waffle, honeycomb, skin stringer, monocoque and other structures. In all cases multiple loading conditions may be applied and typically several failure margins are evaluated to synthesize optimum design definitions. 

 

ISOGRID-SST™ ISOPLT - ISOGRID FLAT PLATES


TEST PANEL BULKHEAD                                       P_7TEST    6 Aug 1999
ALUM 2219-T851 150 F                  Flanged Isogrid             ENGLISH UNITS
Centrally & shear loaded rectangular plate, edges simply supported.
 
GEOMETRY, ANALYSIS CONDITIONS AND RESULTS 
PLATE SIZE: LENGTH, WIDTH              in.         11     25 
 
                                        RESULT     DELTA     MINIMUM   MAXIMUM
 
FLANGE THICKNESS             in.        .25        0         .25       .25 
No. OF LONG. RIBS                       5          1         5         6 
PLATE THICKNESS              in.        1.5        .2        1.3       2 
RIB WIDTH                    in.        .7         .1        .5        .7 
SKIN THICKNESS               in.        .15        .01       .14       .15 
WEB WIDTH                    in.        .08 
NODE-TO-NODE SPACING         in.        5.77 
No. OF EFFECTIVE SKINS                  14.3 
CENTROID TO FLANGE EDGE      in.        .995 
RIB MOMENT OF INERTIA        in^4       .271 
RIB CROSS SECTION AREA       sqin       1.03 
 
CENTRAL LOAD:                                     COMPRESSION
 
LOCAL LOAD,  CONTACT RADIUS                       54000 lbs.       2.5 in.
 
MASS PROPERTIES 
WEIGHT EQUIV. THICKNESS      in.        .34 
WEIGHT PER UNIT AREA         psi        .0347 
WEIGHT OF STRUCTURE          lbs.        9.544 
 
MATERIAL PROPERTIES 
DENSITY                      lbs./cuin   .102 
SHEAR STRENGTH               psi        30200 
SHEAR MODULUS                psi        4.E+6 
ULTIMATE STRENGTH            psi        57000 
YIELD STRENGTH               psi        47000 
YOUNG'S MODULUS              psi        1.06E+7 
 
PLATE STIFFNESS PARAMETERS 
ISO STIFFNESS EQUIV.: MODULUS, THICKNESS    1.24E+6 psi     1.76 in.
LATERAL DEFLECTIONS:   ACTUAL, ALLOWABLE   -.179 in.        1.5 in.
 
SAFETY FACTORS & MARGINS                ULTIMATE  YIELD
 
SAFETY FACTORS                          1.4        1.25     
MARGINS                                 .0865      .00422 
 
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