1 |
Takehumi I. and Mastuo K., 'Mechanics of Shock Wave', 1st edition, Corona, pp. 150-231
|
2 |
Erdos J. I., Bakos R. J., Castro giovanni A., and Rogers, R. C., 1997, 'Dual Mode Shock Expansion/Reflected-Shock Tunnel', AIAA paper 97-0560
|
3 |
Rogers R. C. and Shih A. T., 2001, 'Scramjet Test in a Shock Tunnel at Flight Mach 7, 10, and 15 Conditions', AIAA paper 2001-3241
|
4 |
Cook W. J., Presley L. L. and Chapman G. T., 1980, 'Test Section Configuration for Aerodynamic Testing in Shock tube', Shock Tube and Waves, The Magens Press, pp. 127-136
|
5 |
Amemiya T., Yamaguchi Y., Sekimoto K. and Yamaguchi S., 1992, 'An Experimental study with a shock tube', Proc. Western Division Meeting of Japan Society for Aeronautical and Space Sciences, pp. 29-32
|
6 |
Cook W. J., Presley L. L. and Chapman G. T., 1979, 'Shock Tube as a Device for Testing Transonic Airfoils at High Reynolds Number', AIAA J. Vol. 17, No.7, pp 714 -721
DOI
ScienceOn
|