A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. The basic steps of an algorithm

✍ Scribed by A. V. Gorelov; I. N. Sidorov

• Book ID: 111510642
• Publisher: Allerton Press, Inc.
• Year: 2011
• Tongue: English
• Weight: 601 KB
• Volume: 54
• Category: Article
• ISSN: 1068-7998
• DOI: 10.3103/s1068799811030019