Developing a stress wave thrust balance for a hypersonic shock tunnel
暂无分享,去创建一个
[1] Allan Paull. Hypersonic ignition and thrust production in a scramjet , 1993 .
[2] William J.T. Daniel,et al. Balances for the measurement of multiple components of force in flows of a millisecond duration , 1995 .
[3] Allan Paull,et al. Scramjet thrust measurement in a shock tunnel , 1995 .
[4] H. Grönig,et al. A Six Component Balance for Short Duration Hypersonic Facilities , 1993 .
[5] Mario Carbonaro. Aerodynamic Force Measurements in the VKI Longshot Hypersonic Facility , 1993 .
[6] K. W. Naumann,et al. Millisecond aerodynamic force measurement with side-jet model in theISL shock tunnel , 1993 .
[7] Timothy J. McIntyre,et al. Imaging of Combustion Processes in a Supersonic-combustion Ramjet , 1995 .
[8] Sean Tuttle,et al. Drag measurements at Mach 5 using a stress wave force balance , 1995 .