Material Allowables

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Allowables Ensure the Structural Integrity of the Final Product • Allowables Design Requirements • Static Allowables Properties and Bases • Allowables Development and Publication • Presentation of Design Manuals and Examples of Use Design and Analysis of Aircraft Structures 14-18
Allowables Development Requirements • Program g request q • Firm specification • Test program planning • Specimen fabrication and testing • Allowables development • DDocument t D6 D6-57037, 57037 “P “Procedure d ffor MMaterial t i l Selection and Development of Design/Producibility Data” Design and Analysis of Aircraft Structures 14-19
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 and 10: Allowables Ensure the Structural In
Page 11 and 12: Strength Is an Allowables Domain Me
Page 13 and 14: The Allowable Need is Dependent Upo
Page 15 and 16: Probability Distribution A formula
Page 17: Allowable Need Is Dependent Upon th
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

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