Pre-Test Analysis Predictions for the Shell Buckling Knockdown Factor Checkout Tests - TA01 and TA02

By: Administration (Nasa), National Aeronaut

Technical Report Thornburgh, Robert P. and Hilburger, Mark W. Langley Research Center NASA/TM-2011-216875, ARL-TR-5123, L-19958, NF1676L-11908 WBS 869021.04.07.01.13 STRUCTURAL ANALYSIS; LITHIUM ALLOYS; SHELL STABILITY; CYLINDRICAL SHELLS; ALUMINUM ALLOYS; LOADS (FORCES); CHECKOUT; SEQUENCING; SAFETY

• Format: Paperback
• Language: English
• ISBN: B08F6YD6WK
• ISBN13: 9798673132029
• Release Date: January 1
• Publisher: Independently Published
• Length: 48 Pages
• Weight: 0.30 lbs.
• Dimensions: 0.1" x 8.5" x 11.0"