Aerothermal Performance of a Cooled Winglet at Engine Representative Mach and Reynolds Numbers
Journal of turbomachinery ; 135 , 1 ; 11041-11041
2013
Article (Journal)
English
Aerothermal Performance of a Winglet at Engine Representative Mach and Reynolds Numbers
| Online Contents | 2011
Aerothermal tests of a heat-pipe-cooled leading edge at mach 7
| TIBKAT | 1978
Winglet Effectiveness on Low Aspect Ratio Wings at Supersonic Mach Numbers
| British Library Conference Proceedings | 1991