Aerodynamic investigations of an advanced over-the-wing nacelle transport aircraft configuration

被引：0
|
作者：
Hill, Geoffrey A. [1 ,3 ,4 ]
Kandil, Osama A. [1 ,5 ]
Hahn, Andrew S. [2 ,6 ]
机构：
[1] Old Dominion University, Norfolk, VA 23529, United States
[2] NASA Langley Research Center, Hampton, VA 23681, United States
[3] Department of Aerospace Engineering
[4] 1011 Lockheed Way, Palmdale, CA 93599, United States
[5] Department of Aerospace Engineering, 1300 Elkhorn Avenue, United States
[6] Aeronautics Systems Analysis Branch, Mail Stop 348, United States
来源：
Journal of Aircraft | 2009年 / 46卷 / 01期
关键词：
15;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
Conference article (CA)
引用
收藏
页码：25 / 35
相关论文
共 50 条
  • [31] Optimization of the Aerodynamic Configuration of the Isolated Wing for the Second-Generation Supersonic Passenger Aircraft
    Shirokov M.V.
    Strelets D.Y.
    Bashkirov I.G.
    Russian Aeronautics, 2024, 67 (01): : 70 - 79
  • [32] INVESTIGATIONS OF PROPULSION INTEGRATION INTERFERENCE EFFECTS ON A TRANSPORT AIRCRAFT CONFIGURATION
    ROSSOW, CC
    GODARD, JL
    HOHEISEL, H
    SCHMITT, V
    JOURNAL OF AIRCRAFT, 1994, 31 (05): : 1022 - 1030
  • [33] Investigations of propulsion integration interference effects on a transport aircraft configuration
    Rossow, C.-C.
    Godard, J.-L.
    Hoheisel, H.
    Schmitt, V.
    1600, AIAA, Washington, DC, United States (31):
  • [34] Multi-disciplinary and multi-objective optimization of an over-wing-nacelle aircraft concept
    Gemma S.
    Mastroddi F.
    CEAS Aeronautical Journal, 2019, 10 (03) : 771 - 793
  • [35] Multi-objective wing shape optimization for a wide-body civil aircraft in wing-body-pylon-powered nacelle configuration
    Xue B.
    Zhang W.
    Sun X.
    Wu Y.
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2019, 40 (02):
  • [36] Experimental and numerical investigations of unsteady aerodynamic derivatives for a generic lambda wing UCAV configuration
    Zimper D.
    Huber K.C.
    CEAS Aeronautical Journal, 2020, 11 (02): : 475 - 485
  • [37] Aerodynamic Characteristics Analysis and Capability Assessment of Structural Damaged Aircraft with Advanced Configuration
    Wen, Yang
    Yang, Lingyu
    Shen, Gongzhang
    2011 INTERNATIONAL CONFERENCE ON ELECTRONICS, COMMUNICATIONS AND CONTROL (ICECC), 2011, : 2506 - 2511
  • [38] Aerodynamic Performance of Swayasa Aircraft Wing Model against the Effect of Airfoil Flap Angle Configuration
    Salam, Nasaruddin
    Tarakka, Rustan
    Kasim, Lukman
    Pasau, Kristiana
    INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND ROBOTICS RESEARCH, 2025, 14 (01): : 48 - 58
  • [39] PROPULSIVE AERODYNAMICS OF AN ADVANCED NOZZLE-FORWARD SWEPT WING AIRCRAFT CONFIGURATION
    BOWERS, DL
    JOURNAL OF AIRCRAFT, 1981, 18 (07): : 582 - 586
  • [40] Multi-Point Aerodynamic Design Optimization of DLR F-6 Wing-Body-Nacelle-Pylon Configuration
    Saitoh, Takashi
    Kim, Hyoungjin
    Takenaka, Keizo
    Nakahashi, Kazuhiro
    INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, 2017, 18 (03) : 403 - 413
12345