Design and implementation of an internal stress wave force balance in a shock tunnel [0.03%]
激波风洞内应力波力平衡的设计与实现
M. J. Robinson; J. Martinez Schramm; K. Hannemann
M. J. Robinson; J. Martinez Schramm; K. Hannemann
Study of flow control by localized volume heating in hypersonic boundary layers [0.03%]
高超声速边界层中局部体积加热的流动控制研究
Keller, M. A.; Kloker, M. J.; Kirilovskiy et al.
Keller et al.
Multi-frequency dynamic absorber for improved spacecraft comfort during the launch phase [0.03%]
用于提升航天器发射阶段舒适度的多频动态吸振器
Mastroddi, Franco; Facchini, Gianluca; Gaudenzi et al.
Mastroddi et al.
Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall [0.03%]
热负荷高部件的寿命预测：火箭燃烧室热壁损伤过程的建模
W. Schwarz; S. Schwub; K. Quering; D. Wiedmann; H. W. Höppel; M. Göken
W. Schwarz; S. Schwub; K. Quering; D. Wiedmann; H. W. Höppel; M. Göken
Weak stability boundary transfer to the Moon from GTO as a piggyback payload on Ariane 5 [0.03%]
作为“阿丽亚娜5”火箭的搭载体，从地球同步转移轨道向月球进行弱稳定性边界转移
Quantius, Dominik; Spurmann, Jörn; Dekens et al.
Quantius et al.