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Published byGerard Gardner Modified over 6 years ago
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Steven (“CJ”) Hiu 02/20/2008 Congratulations MAT Coders
Steven (“CJ”) Hiu 02/20/2008 Congratulations MAT Coders! Structural Analysis: Tanks and Intertank Couplers MAT Coder – Structures Acknowledgements: John Tsohas, Prof. Stephen Heister AAE 450 Spring 2008
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Structures Status Report
Good work done so far Current Problems High Inert Mass Fractions Foreseeable problems moving into Phase II Design Added loads on structure (Aero, Thermal, D&C, Avionics) Added mass (Stringers, Baffles, Rings, Couplers, Pipes, Valves, Avionics) Detailed analysis (Welding, Fasteners, Stress Concentrations) 3S mission success and 90% confidence against catastrophic failure Ways Forwards Safeguards in Preliminary Design (RF, conservatism) Clever Design (spun hemicylinders etc) & Analysis (eg Pressure) AAE 450 Spring 2008 Structures
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Weight Saving – Pressurized Monocoque
Bruhn C8 Design curves based on test data 90% confidence curves 15-20% increase in tank strength vs axial buckling (17% in MAT run) 30-40% increase in tank strength vs. bending (potential) Potential weight savings Flight pressure-stabilized design AAE 450 Spring 2008 Structures
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References Bruhn, E, Analysis and Design of Flight Vehicle Structures, 1973 Huzel & Huang, Design of liquid propellant rocket engines, NASA SP-125, 2nd Ed. Megyesy, E, Pressure Vessel Handbook, 10th Ed. Acknowledgements John Tsohas Alan Schwing and Danielle Yaple for Matlab debugging AAE 450 Spring 2008 Structures
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Backup Slide 1 Increase in Axial Buckling Strength Source: Bruhn
Regression Plot of Increase in Compressive Buckling Stress due to Pressure Source: Bruhn C8.11 Source: Bruhn AAE 450 Spring 2008 Structures
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Backup Slide 2 Buckling Strength Bruhn C8.2 Baker Method 3
Unconservative No length effects Baker Method 3 used in tanks Matlab code AAE 450 Spring 2008 Structures
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Backup Slide 3 Bending Strength of Cylindrical Tank
Source: Bruhn Fig C8.13a AAE 450 Spring 2008 AAE 450 Spring 2008 <7> Structures
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Backup Slide 4 Bending Strength with Internal Pressure
Source: Bruhn Fig C8.14 AAE 450 Spring 2008 Structures
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Backup Slide 5 Bruhn A20 Stiffener-strengthened structures in shear and bending Complicated analysis Heavy Expensive to manufacture May be necessary Matlab code 40% complete Source: Bruhn Fig C8.14 AAE 450 Spring 2008
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Backup Slide 6 Weld Efficiencies Weld is stronger than material
Knockdown effect at joins Radiographic Inspection impractical? Need to design stronger part to compensate Source: Megyesevy AAE 450 Spring 2008
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