Material Allowables

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Allowables and Design Value Definitions • Allowables: Mechanical properties having a level of statistical assurance – general case • DDesign i value: l A mechanical property value based on the allowable adapted p to the criteria and analysis y method used – specific case Design and Analysis of Aircraft Structures 14-10
Strength Is an Allowables Domain Mechanical Properties St Strength th properties ti ( (reduced) d d) Ftu, Fty, Fsu Elastic properties (typical) EE, GG, u Physical properties (typical) w, k Design and Analysis of Aircraft Structures 14-11
Page 1 and 2: Material Allowables
Page 3 and 4: Design and Analysis of Aircraft Str
Page 5 and 6: Investigation of Methods and Allowa
Page 7 and 8: Allowables Are Required by FAA to C
Page 9: Allowables Ensure the Structural In
Page 13 and 14: The Allowable Need is Dependent Upo
Page 15 and 16: Probability Distribution A formula
Page 17 and 18: Allowable Need Is Dependent Upon th
Page 19 and 20: Allowables Development Requirements
Page 21 and 22: Allowables Typical Allowables Test
Page 23 and 24: BDM-4090 7075 Design and Analysis o
Page 25 and 26: BDM-4090 7075 Design and Analysis o
Page 27 and 28: Sample Problem • What is the tens
Page 29 and 30: Example Solution Answer = (79 ksi)(
Page 31 and 32: Joint Strength Single Shear Design
Page 33 and 34: Example Solution Design and Analysi
Page 35: Tension Fasteners Design and Analys

Material Allowables

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