共 19 条
- [1] Hinge moment balance technique and application in hypersonic wind tunnel Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2007, 21 (03): : 54 - 57
- [2] Wind Tunnel Balance Development for Ludwieg Tube Facilities AIAA AVIATION FORUM AND ASCEND 2024, 2024,
- [4] Hinge moment balance technique with axial force measurement and its application in wind tunnel test Shiyan Liuti Lixue/Journal of Experiments in Fluid Mechanics, 2011, 25 (02): : 88 - 91
- [5] A new force-measuring balance for large-scale model in hypersonic wind tunnel REVIEW OF SCIENTIFIC INSTRUMENTS, 2021, 92 (11):
- [6] NEW ROTATION-BALANCE APPARATUS FOR MEASURING AIRPLANE SPIN AERODYNAMICS IN THE WIND-TUNNEL JOURNAL OF AIRCRAFT, 1979, 16 (04): : 264 - 268
- [7] Prediction Interval Development for Wind-Tunnel Balance Check-Loading JOURNAL OF AIRCRAFT, 2015, 52 (03): : 884 - 889
- [8] The development of the larger axial force intermediate temperature balance in the hypersonic wind tunnel Shiyan Liuti Lixue, 2006, 1 (86-90):
- [9] Prediction interval development for wind-tunnel balance check-loading 1600, AIAA International, 12700 Sunrise Valley Drive, Suite 200Reston, VA, Virginia, Virginia 20191-5807, United States (52):