High-Fidelity Swept and Leaned Rotor Blade Design Optimization Using Evolutionary Algorithm
- 著者名:
- 掲載資料名:
- A collection of technical papers : 16th AIAA Computational Fluid Dynamics Conference, Orlando, Florida 23-26 June 2003
- シリーズ名:
- AIAA Paper : AIAA Computational Fluid Dynamics Conference
- シリーズ巻号:
- 2003
- 発行年:
- 2003
- 巻:
- v. 3
- 通号:
- 2003-4091
- ペーパー番号:
- AIAA-2003-4091
- 開始ページ:
- 1495
- 終了ページ:
- 1504
- 総ページ数:
- 10
- 出版情報:
- Reston, Va.: American Institute of Aeronautics and Astronautics
- ISBN:
- 9781563475993 [1563475995]
- 言語:
- 英語
- 請求記号:
- A07400/033424 (v.3)
- 資料種別:
- テクニカルペーパー
類似資料:
American Institute of Aeronautics and Astronautics |
7
テクニカルペーパー
Multiobjective Optimization Using Coupled Response Surface Model and Evolutionary Algorithm
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
8
テクニカルペーパー
High-Fidelity Multidisciplinary Design Optimization of Aerostructural Wing Shape for Regional Jet
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
4
テクニカルペーパー
Multiobjective Optimization of a Transonic Compressor Blade Using Evolutionary Algorithm
American Institute of Aeronautics and Astronautics |
American Institute of Aeronautics and Astronautics |
5
テクニカルペーパー
Navier-Stokes Optimization of Supersonic Wings with Four Design Objectives Using Evolutionary Algorithm
American Institute of Aeronautics and Astronautics |
American Society of Mechanical Engineers |
American Institute of Aeronautics and Astronautics |
12
テクニカルペーパー
Improvement of Nonlinear Lateral Characteristics of Lifting-Body Type Reentry Vehicle Using Optimization Algorithm
American Institute of Aeronautics and Astronautics |