How to Design Tapered Sections for Flexural Members?

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Discussion Overview

The discussion focuses on the design of tapered sections for flexural members in structural engineering. Participants explore how to calculate deflection and allowable compressive bending stress in these members, considering both theoretical and practical aspects of beam analysis.

Discussion Character

  • Technical explanation, Conceptual clarification, Debate/contested

Main Points Raised

  • One participant seeks guidance on designing tapered sections as flexural members, specifically regarding deflection calculations and allowable compressive bending stress.
  • Another participant inquires if the original poster is referring to tapered beams and suggests consulting Machinery's Handbook for relevant data.
  • A participant emphasizes that basic beam analysis principles apply, noting that the cross-sectional moment of inertia will vary along the beam and that integration may be necessary for accurate results.
  • There is a suggestion that for complex structures, numerical analysis might be required to address the design challenges posed by tapered sections.

Areas of Agreement / Disagreement

Participants have not reached a consensus, and multiple perspectives on the design and analysis of tapered sections remain. Some participants provide suggestions while others seek further clarification.

Contextual Notes

The discussion does not clarify specific assumptions regarding material properties, loading conditions, or the complexity of the tapered sections being analyzed, which may affect the design approach.

hpsmahal
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Hi there

Am basically a structural Engineer I got struck while Designing the Tapered Section. I want to know how these members should be designed as a flexural members. how can I calculate the deflection in these members & allowable compressive bending stress.
 
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Are you asking about tapered beams? Do you have access to Machinery's Handbook?
 
yes i am talkig about tappered sections. Are you having relevant data for that.
Thanx
 
What is there to really know? Do you have anything in your background regarding beam loading? Basic beam analysis would still hold true except now the cross sectional moment of inertia is going to be a function of distance along the beam. You'll have to integrate to get the results. Of course, if you're talking about a complicated structure then you'll need numerical analysis.
 

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