Jan 9, 2006 #1 rob768 Mechanical Joined Aug 3, 2005 Messages 441 Location NL Can anyone direct me to a site with information of fatigue properties of steel type 34 CrNiMo 6? tnx
Jan 16, 2006 #2 Goahead Aerospace Joined Jul 13, 2003 Messages 625 Location IL You might be able to find pertinent answers with european steel manufacturers. Or by browsing the results of a Google Search: see for example: http://www.ingentaconnect.com/content/els/01678442/2001/00000035/00000001 Regards, http://www.welding-advisers.com/ Upvote 0 Downvote
You might be able to find pertinent answers with european steel manufacturers. Or by browsing the results of a Google Search: see for example: http://www.ingentaconnect.com/content/els/01678442/2001/00000035/00000001 Regards, http://www.welding-advisers.com/
Jan 16, 2006 #3 Carburize Materials Joined Sep 23, 2002 Messages 702 Location US At equivalent strength levels this material has very similar fatigue properties to 4340. Upvote 0 Downvote
Jan 16, 2006 Thread starter #4 rob768 Mechanical Joined Aug 3, 2005 Messages 441 Location NL do you have fatigue details of that material? Upvote 0 Downvote
Jan 17, 2006 #5 Carburize Materials Joined Sep 23, 2002 Messages 702 Location US There is a bunch of data on 4340 in "Atlas of Fatigue Curves" Published by ASM and ASM Handbook Volume 19 "Fatigue and Fracture" Upvote 0 Downvote
There is a bunch of data on 4340 in "Atlas of Fatigue Curves" Published by ASM and ASM Handbook Volume 19 "Fatigue and Fracture"
Jan 17, 2006 #6 TVP Materials Joined Apr 12, 2002 Messages 4,592 Location US MIL-HDBK-5J (or -5H) and its successor DOT/FAA/AR-MMPDS-01 both have fatigue data for 4340. Use the following links to obtain them: http://assist.daps.dla.mil/eAccess/index.cfm?ident_number=53876 http://www.airplanedesign.aero/inde...40&;func=fileinfo&filecatid=3&parent=category Upvote 0 Downvote
MIL-HDBK-5J (or -5H) and its successor DOT/FAA/AR-MMPDS-01 both have fatigue data for 4340. Use the following links to obtain them: http://assist.daps.dla.mil/eAccess/index.cfm?ident_number=53876 http://www.airplanedesign.aero/inde...40&;func=fileinfo&filecatid=3&parent=category