THE COMPRESSIBILITY RULE FOR DRAG OF AIRFOIL NOSES

被引:0
|
作者
JONES, RT
VANDYKE, MD
机构
来源
JOURNAL OF THE AERONAUTICAL SCIENCES | 1958年 / 25卷 / 03期
关键词
D O I
10.2514/8.7560
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
引用
收藏
页码:171 / &
相关论文
共 50 条
  • [31] Comment on "Compressibility and Rarefaction Effects on Drag of a Spherical Particle"
    Harrison, Alan K.
    AIAA JOURNAL, 2021, 59 (08) : 3288 - 3289
  • [32] APPLICATION OF OSWATITSCHS THEOREM TO SUPERCRITICAL AIRFOIL DRAG CALCULATION
    INGER, GR
    JOURNAL OF AIRCRAFT, 1993, 30 (03): : 415 - 417
  • [33] Drag reduction due to riblets on a GAW(2) airfoil
    Subaschandar, N
    Kumar, R
    Sundaram, S
    JOURNAL OF AIRCRAFT, 1999, 36 (05): : 890 - 892
  • [34] Drag Reduction by Uniform Blowing on the Pressure Surface of an Airfoil
    Miura, Senri
    Ohashi, Masahiro
    Fukagata, Koji
    Tokugawa, Naoko
    AIAA JOURNAL, 2021, : 2241 - 2250
  • [35] Drag reduction due to riblets on a GAW(2) airfoil
    Subaschandar, N.
    Kumar, Rajeev
    Sundaram, S.
    Journal of Aircraft, 36 (05): : 890 - 892
  • [36] High-Incidence Airfoil Lift and Drag Estimates
    Traub, Lance W.
    JOURNAL OF AIRCRAFT, 2012, 49 (01): : 311 - 314
  • [37] Actively Reduced Airfoil Drag by Transversal Surface Waves
    Albers, Marian
    Meysonnat, Pascal S.
    Schroeder, Wolfgang
    FLOW TURBULENCE AND COMBUSTION, 2019, 102 (04) : 865 - 886
  • [38] On Drag Reduction Effect of Contour Bump of supercritical Airfoil
    Tao Yang
    Liu Guangyuan
    Wang Hongbiao
    Wang Yuanjing
    Zhao Zhong-liang
    2013 FOURTH INTERNATIONAL CONFERENCE ON DIGITAL MANUFACTURING AND AUTOMATION (ICDMA), 2013, : 879 - 882
  • [39] Airfoil Lift and Drag Extrapolation with Viterna and Montgomerie Methods
    Mahmuddin, Faisal
    Klara, Syerly
    Sitepu, Husni
    Hariyanto, Surya
    8TH INTERNATIONAL CONFERENCE ON APPLIED ENERGY (ICAE2016), 2017, 105 : 811 - 816
  • [40] Wave drag reduction of airfoil with shock control bump
    Li, Peifeng
    Zhang, Binqian
    Chen, Yingchun
    Chen, Zhenli
    Hangkong Xuebao/Acta Aeronautica et Astronautica Sinica, 2011, 32 (06): : 971 - 977