Design and analysis of a flat accelerometer-based force balance system for shock tunnel testing
暂无分享,去创建一个
Gopalan Jagadeesh | Kpj Reddy | D. R. Mahapatra | Niranjan Sahoo | Srinivasan Gopalakrishnan | G. Jagadeesh | K. Reddy | S. Gopalakrishnan | N. Sahoo | D. Mahapatra
[1] K. W. Naumann,et al. Millisecond aerodynamic force measurement with side-jet model in theISL shock tunnel , 1993 .
[2] Gopalan Jagadeesh,et al. An accelerometer balance system for measurement of aerodynamic force coefficients over blunt bodies in a hypersonic shock tunnel , 2003 .
[3] William H. Rae,et al. Low-Speed Wind Tunnel Testing , 1966 .
[4] M. V. Joshi,et al. Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ = 5.5 , 1986 .
[5] S R Sanderson,et al. Drag balance for hypervelocity impulse facilities , 1991 .
[6] Patrick Gnemmi,et al. High-Pressure Shock Tunnel Experiments and CFD Calculations on Spike-Tipped Blunt Bodies , 2002 .
[7] Bernd F. R. Ewald,et al. REVIEW ARTICLE: Multi-component force balances for conventional and cryogenic wind tunnels , 2000 .
[8] Kirk S. Schanze,et al. Pressure-sensitive paint measurements in a shock tube , 2000 .
[9] N. M. Reddy,et al. Aerodynamic force measurements over missile configurations in IISc shock tunnel at M∞ =3.85 and 9.15 , 1990 .
[10] George R. Duryea,et al. An Improved Piezoelectric Balance for Aerodynamic Force , 1968, IEEE Transactions on Aerospace and Electronic Systems.