The precision and accuracy of wind tunnel free-flight experiment result

被引:0
|
作者
Jia, Qu-Yao [1 ]
Yang, Yi-Nong [1 ]
Jiang, Zeng-Hui [1 ]
机构
[1] China Institute of Aerodynamics, Beijing 100074, China
来源
Yuhang Xuebao/Journal of Astronautics | 2009年 / 30卷 / 06期
关键词
Free flight - Gas dynamics - Wind tunnels;
D O I
10.3873/j.issn.1000-1328.2009.06.005
中图分类号
学科分类号
摘要
Wind tunnel free-flight experiment is especial wind tunnel experiment aground. We, the only one throughout the country, have conducted the research of unsteady aerodynamic characteristics of several aerocrafts at 0.6~6.0 mach and up to 45 kilometers of altitude by wind tunnel free-flight experiment. Thus the accuracy and reliability of wind tunnel free-flight experiment should be provided. The accord between flight and wind tunnel experiment is the most important criterion of assessing accuracy and reliability of experiment result.
引用
收藏
页码:2082 / 2085
相关论文
共 50 条
  • [31] Accurate position control of a flapping-wing robot enabling free-flight flow visualisation in a wind tunnel
    Karasek, Matej
    Percin, Mustafa
    Cunis, Torbjorn
    van Oudheusden, Bas W.
    De Wagter, Christophe
    Remes, Bart D. W.
    de Croon, Guido C. H. E.
    INTERNATIONAL JOURNAL OF MICRO AIR VEHICLES, 2019, 11
  • [32] Hypersonic wind tunnel free-flight test with biplanar optical system on the non-spinning blunt cone
    China Academy of Aerospace Aerodynamics, Beijing
    100074, China
    Lixue Xuebao, 3 (406-413): : 406 - 413
  • [33] EQUIPMENT WILL NOT PREVENT FREE-FLIGHT
    DORNHEIM, MA
    AVIATION WEEK & SPACE TECHNOLOGY, 1995, 143 (05): : 46 - 46
  • [34] EASE UP ON FREE-FLIGHT
    HALL, G
    AVIATION WEEK & SPACE TECHNOLOGY, 1995, 143 (13): : 6 - 6
  • [35] FREE-FLIGHT BEGS QUESTIONS
    EKINS, J
    AVIATION WEEK & SPACE TECHNOLOGY, 1995, 143 (10): : 6 - 6
  • [36] Aircraft Free Flight Simulation in a Wind Tunnel
    Elhashani, Atahir
    Kurban, Adel
    Agela, Marwa L.
    ENGINEERING AND MANUFACTURING TECHNOLOGIES, 2014, 541-542 : 1390 - 1393
  • [37] Free-flight measurement technique in the free-piston high-enthalpy shock tunnel
    Tanno, H.
    Komuro, T.
    Sato, K.
    Fujita, K.
    Laurence, S. J.
    REVIEW OF SCIENTIFIC INSTRUMENTS, 2014, 85 (04):
  • [39] Nitric oxide molecular tagging velocimetry of a free-flight model in a reflected shock tunnel
    Jans, E.R.
    Lynch, K.P.
    Daniel, K.A.
    Kearney, S.P.
    Optics Letters, 2025, 50 (06) : 1839 - 1842
  • [40] An evolutive environment for development of free-flight
    Oliveira, I
    Cugnasca, P
    Camargo, J
    Fonseca, R
    Silva, J
    PROBABILISTIC SAFETY ASSESSMENT AND MANAGEMENT, VOL 1- 6, 2004, : 513 - 518