✦ LIBER ✦

Reliability analysis of inclined loaded piles using a high-order response surface

✍ Scribed by Chong, Jiang; Minghua, Zhao; Keping, Zhou

Book ID: 126734126
Publisher: Informa UK (Taylor & Francis)
Year: 2014
Tongue: English
Weight: 238 KB
Volume: 18
Category: Article
ISSN: 1964-8189
DOI: 10.1080/19648189.2014.911120

No coin nor oath required. For personal study only.

📜 SIMILAR VOLUMES

Probabilistic analysis of laterally load

Probabilistic analysis of laterally loaded piles using response surface and neural network approaches

✍ Chin Loong Chan; Bak Kong Low 📂 Article 📅 2012 🏛 Elsevier Science 🌐 English ⚖ 610 KB

Reliability-Based Underseepage Analysis

Reliability-Based Underseepage Analysis in Levees Using a Response Surface–Monte Carlo Simulation Method

✍ Rice, John D.; Polanco, Lourdes 📂 Article 📅 2012 🏛 American Society of Civil Engineers 🌐 English ⚖ 994 KB

A new look at the response surface metho

A new look at the response surface method for reliability analysis using chaos theory

✍ Youliang Ding; Aiqun Li; Yang Deng 📂 Article 📅 2008 🏛 Institute of Engineering Mechanics, China Earthqua 🌐 English ⚖ 491 KB

Reliability Analysis of a Composite Plat

Reliability Analysis of a Composite Plate under Low-Velocity Impact using the Gaussian Response Surface Method

✍ Patel, S. D.; Ahmad, S.; Mahajan, P. 📂 Article 📅 2014 🏛 Taylor and Francis Group 🌐 English ⚖ 663 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics 8th AIAA/CEAS Aeroacoustics Conference & Exhibit - Breckenridge, Colorado (17 June 2002 - 19 June 2002)] 8th AIAA/CEAS Aeroacoustics Conference & Exhibit - Nonlinear Analysis of Airfoil High-Intensity Gust Response Using a High-Order Prefactored Compact Code

✍ Crivellini, Andrea; Golubev, Vladimir; Mankbadi, Reda; Scott, James; Hixon, Ray; 📂 Article 📅 2002 🏛 American Institute of Aeronautics and Astronautics ⚖ 811 KB

[American Institute of Aeronautics and A

[American Institute of Aeronautics and Astronautics AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum - Los Angeles, California (01 October 2002 - 03 October 2002)] AIAA's Aircraft Technology, Integration, and Operations (ATIO) 2002 Technical Forum - Using Response Surface Equations to Optimize the Aerodynamics of a High Speed Standoff Missile Within a Multi-Disciplinary Analysis Setting

✍ Won, Henry; Pfaender, Jens Holger; Levine, Simon; Mavris, Dimitri 📂 Article 📅 2002 🏛 American Institute of Aeronautics and Astronautics ⚖ 724 KB