Development and characterization of a low-cost wind tunnel balance for aerodynamic drag measurements

被引:2
|
作者
Sor, Suthyvann [1 ]
Bardera, Rafael [1 ]
Garcia-Magarino, Adelaida [1 ]
Matias Garcia, Juan Carlos [1 ]
Donoso, Eduardo [2 ]
机构
[1] INTA, Expt Aerodynam, Madrid, Spain
[2] Univ Politecn Madrid, ETSIAE, Madrid, Spain
关键词
balance; load cell; balance calibration; drag coefficient; wind tunnel; FORCE BALANCE; DESIGN; SIMULATION; SYSTEM;
D O I
10.1088/1361-6404/ab1a7b
中图分类号
G40 [教育学];
学科分类号
040101 ; 120403 ;
摘要
Drag force measurement is one of the most important data that can be obtained in wind tunnel tests. Drag force is directly related to the energy that a vehicle needs to move, and, therefore, to the fuel costs associated with it. For vehicles, drag forces are usually measured in wind tunnels. The typical instruments for drag measurement are the force balances, which are usually complex and expensive instruments. The aim of this investigation is to study the development of a low-cost in-house balance for drag measurements in a wind tunnel. Based on a commercial available load cell XFTC300 Series in combination with simple elements designed and manufactured at INTA, a balance capable of measuring the drag force to models in a considerably wide adjustable range has been developed and characterized. The balance has been calibrated and used in a wind tunnel. Tests were carried out on a truck model, a simplified frigate shape and an Ahmed Body to obtain the resistance coefficient and evaluate the operation of the balance.
引用
收藏
页数:27
相关论文
共 50 条
  • [21] Aerodynamic Characteristics of Busemann Biplane by Wake Measurements in Low-Speed Wind Tunnel
    Kashitani, Masashi
    Thai Duong Nguyen
    Kusunose, Kazuhiro
    Taguchi, Masato
    Takita, Yoshihiro
    TRANSACTIONS OF THE JAPAN SOCIETY FOR AERONAUTICAL AND SPACE SCIENCES, 2021, 64 (05) : 258 - 266
  • [22] Development of a Wind Tunnel Test Section for Evaluation of Heavy Vehicle Aerodynamic Drag at a scale of 1:3
    McArthur, Damien J.
    Burton, David
    Thompson, Mark
    Sheridan, John
    SAE INTERNATIONAL JOURNAL OF COMMERCIAL VEHICLES, 2013, 6 (02) : 522 - 528
  • [23] DESIGN OF A LOW-COST STRATIFIED BOUNDARY-LAYER WIND-TUNNEL
    SCHATZMANN, M
    DONAT, J
    HENDEL, S
    KRISHAN, G
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1995, 54 : 483 - 491
  • [24] A SENSITIVE AERODYNAMIC DRAG BALANCE AS AN INDICATOR OF LOW AIR SPEEDS
    KEMP, JF
    JOURNAL OF SCIENTIFIC INSTRUMENTS, 1957, 34 (10): : 411 - 415
  • [25] Tunnel face videogrammetry for low-cost digitization and discontinuity set orientation measurements
    Janiszewski, M.
    Torkan, M.
    Uotinen, L.
    Javed, H.
    Rinne, M.
    NEW CHALLENGES IN ROCK MECHANICS AND ROCK ENGINEERING, EUROCK 2024, 2024, : 872 - 878
  • [26] WIND-TUNNEL ERRORS IN DRAG MEASUREMENTS OF POWER CONDUCTORS
    BALL, NG
    RAWLINS, CB
    RENOWDEN, JD
    JOURNAL OF WIND ENGINEERING AND INDUSTRIAL AERODYNAMICS, 1992, 41 (1-3) : 847 - 857
  • [27] Aerodynamic performance of a low-speed wind tunnel
    Frechen, FB
    Frey, M
    Wett, M
    Löser, C
    WATER SCIENCE AND TECHNOLOGY, 2004, 50 (04) : 57 - 64
  • [28] LOW-COST NANOSCALE MEASUREMENTS
    不详
    CHEMICAL & ENGINEERING NEWS, 2008, 86 (47) : 42 - 42
  • [29] AERODYNAMIC MEASUREMENTS ON A VERTICAL AXIS WIND TURBINE IN A LARGE SCALE WIND TUNNEL
    Battisti, L.
    Zanne, L.
    Dell'Anna, S.
    Dossena, V.
    Paradiso, B.
    Persico, G.
    PROCEEDINGS OF THE ASME TURBO EXPO 2010, VOL 5, 2010, : 891 - 900
  • [30] Aerodynamic Measurements on a Vertical Axis Wind Turbine in a Large Scale Wind Tunnel
    Battisti, L.
    Zanne, L.
    Dell'Anna, S.
    Dossena, V.
    Persico, G.
    Paradiso, B.
    JOURNAL OF ENERGY RESOURCES TECHNOLOGY-TRANSACTIONS OF THE ASME, 2011, 133 (03):