Dec 30, 2010 #1 Apsu Aerospace Joined Dec 30, 2010 Messages 10 Location GB Does any one know of a method to design a gas turbine or compressor blade so that under a combined tension (CF) and gas bending load the traditional located stress peaks at LE,TE and Blade to Platform are avoided.
Does any one know of a method to design a gas turbine or compressor blade so that under a combined tension (CF) and gas bending load the traditional located stress peaks at LE,TE and Blade to Platform are avoided.
Dec 30, 2010 #2 rb1957 Aerospace Joined Apr 15, 2005 Messages 16,167 Location CA simultaneous posting is not allowed ... Upvote 0 Downvote
Dec 31, 2010 #3 johnhors Aerospace Joined Jan 21, 2004 Messages 1,021 Location GB You could try contacting Jura Carbon Limited (in the UK), I believe that they have developed such a blade design or something similar. http://www.Roshaz.com Upvote 0 Downvote
You could try contacting Jura Carbon Limited (in the UK), I believe that they have developed such a blade design or something similar. http://www.Roshaz.com