Design of a Basic Airfoil for a Slightly Swept Wing. Part 1: Theoretical Transonic Airfoil Design.

被引：0
|
作者：
Wichmann, Georg
机构：
来源：
| 1600年
关键词：
D O I：
暂无
中图分类号：
学科分类号：
摘要：
15
引用
收藏
相关论文
共 50 条
  • [21] Response surface method for airfoil design in transonic flow
    Ahn, J
    Kim, HJ
    Lee, DH
    Rho, OH
    JOURNAL OF AIRCRAFT, 2001, 38 (02): : 231 - 238
  • [22] Integrated design methods as components of an expert system for transonic airfoil design
    Zores, Robert
    Forschungsbericht - Deutsche Forschungsanstalt fuer Luft - und Raumfahrt e.V., 1999, 99 (09): : 7 - 124
  • [23] Multi-objective optimization design of airfoil and wing
    Zhu, ZQ
    Fu, HY
    Yu, RX
    Liu, J
    SCIENCE IN CHINA SERIES E-TECHNOLOGICAL SCIENCES, 2004, 47 (01): : 15 - 25
  • [24] Multi-objective optimization design of airfoil and wing
    and WingZHU Ziqiang
    Science in China(Series E:Technological Sciences), 2004, (01) : 15 - 25
  • [25] Multi-objective optimization design of airfoil and wing
    Ziqiang Zhu
    Hongyan Fu
    Rixin Yu
    Jie Liu
    Science in China Series E: Technological Sciences, 2004, 47 : 15 - 25
  • [26] Airfoil and wing design through hybrid optimization strategies
    Ctro. Italiano Ricerche Aerospaziali, 81043 Capua, Italy
    AIAA J, 5 (634-641):
  • [27] Airfoil and wing design through hybrid optimization strategies
    Vicini, A
    Quagliarella, D
    AIAA JOURNAL, 1999, 37 (05) : 634 - 641
  • [28] Airfoil Design and Numerical Analysis for Morphing Wing Structure
    Dong Wenjun
    Sun Qin
    MACHINERY, MATERIALS SCIENCE AND ENGINEERING APPLICATIONS, PTS 1 AND 2, 2011, 228-229 : 169 - +
  • [29] Transonic airfoil design optimization using soft computing methods
    Tse, Daniel
    Chan, Louis
    Canadian Aeronautics and Space Journal, 2000, 46 (02): : 65 - 73
  • [30] The Drag Reduction Design for Transonic Airfoil with Consideration of Laminar Transition
    Wang Long
    Song Wenping
    Zhang Kun
    Yang Xudong
    PROCEEDINGS OF 2010 ASIA-PACIFIC INTERNATIONAL SYMPOSIUM ON AEROSPACE TECHNOLOGY, VOL 1 AND 2, 2010, : 279 - 282
12345