Continue to Site

Eng-Tips is the largest engineering community on the Internet

Intelligent Work Forums for Engineering Professionals

  • Congratulations cowski on being selected by the Eng-Tips community for having the most helpful posts in the forums last week. Way to Go!

Search results for query: *

  • Users: stressebookllc
  • Content: Threads
  • Order by date
  1. stressebookllc

    Pull Away Load on L Bracket Top Leg - Hand Calculation

    Dear Friends, I have a bracket, a simple L bracket, with a couple of fasteners holding it down at the bottom base leg, and a horizontal pull away load at the top leg. I am trying to figure out the reactions with hand calculations. Two other scenarios are fairly straight forward statically...
  2. stressebookllc

    How do aerospace manufacturing companies certify their processes with the FAA?

    As we all know, the FAA needs approved process specifications for mass produced parts used on multiple aircraft. I wrote a little bit I know about this. Process Specifications are critical for a product's consistent quality, and thus 14 CFR compliance and certification...
  3. stressebookllc

    Online Finite Element Analysis Courses

    thread727-216366 I was wondering which online finite element analysis courses you have taken, specifically which ones were good value for your money and why you thought so? Aerospace Stress Analysis and FEA Courses http://www.stressebook.com Stressing Stresslessly!
  4. stressebookllc

    Spring Element Forces in Nastran

    One of the confusing aspects to me was the signs of the induced forces in various types of spring elements: So, a positive spring force is always tension, right? Well..... I found out not really, so i kind of summarized a few things here: http://www.stressebook.com/spring-element-forces/...
  5. stressebookllc

    Plate and Laminate Element Offsets

    Dear Learned Colleagues: I have seen some threads related to plate and laminate element offsets and decided to discuss the topic in some detail here: http://www.stressebook.com/plate-and-laminate-element-offsets1/ But I was wondering if you have any more suggestions to improve the study I...
  6. stressebookllc

    14-cfr-subpart-c-section-25-307

    Proof of Structure, hopefully you can learn something useful and new: http://www.stressebook.com/14-cfr-subpart-c-section-25-307/ Aerospace Stress Analysis and FEA Courses http://www.stressebook.com Stressing Stresslessly!
  7. stressebookllc

    14 CFR Subpart C Section 25-305

    Friends, I'd like to know if you have any useful comments or suggestions on how you have interpreted this regulation. I wrote about it here: http://www.stressebook.com/14-cfr-subpart-c-section-25-305/ Would be nice to know your thoughts as well. Aerospace Stress Analysis and FEA Courses...
  8. stressebookllc

    Shell Element Forces and Moments

    Dear Friends, Most of us are familiar with the membrane forces and shell element moments which are element forces and moments written out as running loads and moments to the output file (.f06 or .out files depending on the flavor of Nastran) General notation is NX NY NXY (membrane forces)...
  9. stressebookllc

    Normal Modes, mass density or weight density?

    In a normal modes analysis, do you use PARAM WTMASS all the time or are there instances where you choose to use weight density? Param WTMASS is generally set to 1/386.4 in english units. It converts the material densities to mass density when you use weight density in the material definition...
  10. stressebookllc

    CBUSH Vs CROD/CVISC Vs CELAS2

    I wrote a blog post on these comparisons at http://www.stressebook.com/spring-elements-in-nastran/ but I'd love to know how creatively you have used them in a challenging modeling scenario. www.stressebook.com Stressing Stresslessly!
  11. stressebookllc

    Primary Structures Stress or Cabin Interiors Stress or Nacelle Stress?

    Some people think that aircraft cabin interiors stress engineering is dumbed down furniture stuff and low tech. But primary structure and nacelle stuff is high tech. What is your opinion? www.stressebook.com Stressing Stresslessly!
  12. stressebookllc

    Plate Bending FEM Convergence Study Vs Theoretical Mc/I

    Dear Friends, I am in the process of double checking a simply supported 10" x 4" plate, supported at the 1.0" from the short edges. The edges are only constrained along TZ. A weak spring is used right in the middle to avoid any fatal errors. Then I used three different mesh sizes to look at the...
  13. stressebookllc

    Aerospace Fitting Section Analysis and Failure Theory

    Dear Friends, one of my subscribers had an interesting question. There are 5 failure theories for metals: 1) Maximum Principal Stress 2) Maximum Principal Strain 3) Maximum shear stress 4) Total strain energy 5) Shear Strain Energy or Distortion Energy (Von Mises) We know Aluminum is...

Part and Inventory Search