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  1. 39minuteman

    Oh, there are jobs... just 5-10 years exp. jobs!

    I'm looking to move to Canada, so I'm watching jobs there for some time. And it's same situation in my field (aeronautical engineering). Almost all positions require more then 5 years of exp. It's all about job market. When I type keywords in job search engine like monster, I usually get 4 to 5...
  2. 39minuteman

    Good text editor for Nastran Deck?

    You could try Notepad++. It's free and I can give you file with Nastran highlighting scheme for it. It works well. http://notepad-plus.sourceforge.net/uk/site.htm
  3. 39minuteman

    Personal Email prohibited at work

    MiketheEngineer, it's a fact that you don't get many responses during the weekend. [blush]
  4. 39minuteman

    Conditions for training of employees

    This is based on fact that this company had several offices across the Europe, but only office in Eastern Europe had such “unique” terms. Further, this “training” lasted only week or two, it was held by company engineers (not by expensive 3rd party expert) and it was more an introduction lecture...
  5. 39minuteman

    Conditions for training of employees

    I had similiar contractual obligations on my first job in company based in Eastern Europe. I received some training at the begining of my employment, but I had to sign that I would stay in company for next 3 years or pay roughly 1 year salary. I considered then, as I consider now, this as very...
  6. 39minuteman

    Linear Finite Element Analysis & NeuberÆs Rule

    Regarding applicability of Neuber's rule jetmaker, you said that this rule can be applied to any region of "local" stress which would result in plastic deformation. It's my understanding that Neuber's rule could be applied only on geometrical discontinuities, ie notches or open holes. In...
  7. 39minuteman

    NASTRAN/FEA GUIDELINES FOR AEROSTRUCTURES?

    I have a set of informal notes which was (supposedly) written by Ian Taig in mid 80-ties. Advices given there are very practical and I believe that most of them are still valid. I put file on engineering.com Enjoy...
  8. 39minuteman

    load distribution along wing spars

    You could also check this post, as some general discussion regarding wing load could be found there http://www.eng-tips.com/viewthread.cfm?qid=143930&page=1 But as 40818 said: Keep it simple. Good luck :)
  9. 39minuteman

    Fatigue damage due to compressive load

    First, thank you all for your valuable responses. der8110 I believe that you are referring to method based on fracture mechanics, in which is common to assume that some initial flaw already exists in the material. However, my understanding is that fatigue crack could develop in “flawless”...
  10. 39minuteman

    Fatigue damage due to compressive load

    I have a question regarding fatigue damage done by compressive-compressive load. I believe that common approach is to consider only load cycles in which max stress is greater then zero. In other words, assumption is made that compressive-compressive cases (both max and min stresses are...

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