AERO STRUCTURAL ANALYS I
AERO STRUCTURAL ANALYS I AERO 304
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This 1 page Class Notes was uploaded by Wilber Bradtke on Wednesday October 21, 2015. The Class Notes belongs to AERO 304 at Texas A&M University taught by Vikram Kinra in Fall. Since its upload, it has received 44 views. For similar materials see /class/226160/aero-304-texas-a-m-university in Aerospace Engineering at Texas A&M University.
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Date Created: 10/21/15
42 Given The prismatic cantilever beam with rectangular cross section shown below 1330x106 psi T 15 in 15 in 100 in x 4 1000 lb 1000 lb Required a Find P Vy V2 Mx My and Mz versus x measured about the geometric centroid and graph these results b Evaluate ouxyz and enxyz c Find the axial stress and strain at the following locations 1 xyz 030 2 xyz 0 30 3 xyz 0015 4 xyz 00 15 7 77 i 7 7 777777gim J6 Given A cantilever beam is loaded as shown below 100 psi 15 in y lt 15 in 1000 lb E 10 X 106 psi 05 in 05 in a 10 x10 60F Required a Draw P V VI MI My and M2 versus x diagrams b Suppose the beam is simultaneously heated AT 100 F at all points Find onxyz c Locate the point where on attains its maximum absolute value and evaluate an at this point Q