FUEL SAVINGS FROM TRUCK AERODYNAMIC DRAG REDUCERS AND CORRELATION WITH WIND-TUNNEL DATA

被引:3
|
作者
BUCKLEY, FT
WALSTON, WH
MARKS, CH
机构
来源
JOURNAL OF ENERGY | 1978年 / 2卷 / 06期
关键词
D O I
10.2514/3.62383
中图分类号
TE [石油、天然气工业]; TK [能源与动力工程];
学科分类号
0807 ; 0820 ;
摘要
引用
收藏
页码:321 / 329
页数:9
相关论文
共 50 条
  • [1] WIND TUNNEL INVESTIGATION INTO THE FUEL SAVINGS AVAILABLE FROM THE AERODYNAMIC DRAG REDUCTION OF TRUCKS.
    Cooper, K.R.
    National Research Council of Canada, Quarterly Bulletin of the Division of Mechanical Engineering, 1976, (03): : 31 - 87
  • [2] WIND-TUNNEL INVESTIGATION OF DEVICES TO REDUCE BUS AERODYNAMIC DRAG
    RAYMER, DP
    ASTRONAUTICS & AERONAUTICS, 1977, 15 (10): : B10 - B10
  • [3] AERODYNAMIC PARAMETERS ESTIMATED FROM FLIGHT AND WIND-TUNNEL DATA
    KLEIN, V
    BATTERSON, JG
    JOURNAL OF AIRCRAFT, 1986, 23 (04): : 306 - 312
  • [4] A wind-tunnel study of windbreak drag
    Guan, DX
    Zhang, YS
    Zhu, TY
    AGRICULTURAL AND FOREST METEOROLOGY, 2003, 118 (1-2) : 75 - 84
  • [5] WIND-TUNNEL CUTS SKIERS DRAG
    不详
    SCIENCE DIGEST, 1983, 91 (12) : 19 - 19
  • [6] CFD Correlation with Wind-Tunnel for Dry Van Trailer Aerodynamic Devices
    Dasarathan, Devaraj
    Ellis, Matthew
    Chinnamani, Surya
    Ayala, Ray
    Haws, James
    SAE INTERNATIONAL JOURNAL OF COMMERCIAL VEHICLES, 2016, 9 (02) : 83 - 93
  • [7] MEASUREMENTS OF WIND DRAG ON PEOPLE STANDING IN A WIND-TUNNEL
    PENWARDEN, AD
    GRIGG, PF
    RAYMENT, R
    BUILDING AND ENVIRONMENT, 1978, 13 (02) : 77 - 84
  • [8] Nonlinear Unsteady Aerodynamic Modeling Using Wind-Tunnel and Computational Data
    Murphy, Patrick C.
    Klein, Vladislav
    Frink, Neal T.
    JOURNAL OF AIRCRAFT, 2017, 54 (02): : 659 - 683
  • [9] INDUCED DRAG OF A WING IN A CIRCULAR WIND-TUNNEL
    YAMAMOTO, Y
    AIAA JOURNAL, 1992, 30 (09) : 2344 - 2346
  • [10] X-33 aerodynamic computations and comparisons with wind-tunnel data
    Hollis, BR
    Thompson, RA
    Murphy, KJ
    Nowak, RJ
    Riley, CJ
    Wood, WA
    Alter, SJ
    Prabhu, RK
    JOURNAL OF SPACECRAFT AND ROCKETS, 2001, 38 (05) : 684 - 691