A lower bound estimate of the critical load for helicopter main rotor composite blade according to the limit equilibrium theory. Analysis results

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

• Book ID: 115065690
• Publisher: Allerton Press, Inc.
• Year: 2011
• Tongue: English
• Weight: 238 KB
• Volume: 54
• Category: Article
• ISSN: 1068-7998
• DOI: 10.3103/s1068799811040039