Flame response to acoustic excitation in a rectangular rocket combustor with LOx/H2propellants [0.03%]
LOx/H2推进剂矩形火箭燃烧室内声激励下的火焰响应
Justin Hardi; Michael Oschwald; Bassam Dally
Justin Hardi; Michael Oschwald; Bassam Dally
Detlef Müller-Wiesner; Rolf Henke; Constantinos Stavrinidis
Detlef Müller-Wiesner; Rolf Henke; Constantinos Stavrinidis
Real-time capable trajectory synthesis via multivariate interpolation methods for a moon landing manoeuvre [0.03%]
基于多元插值方法的月球着陆机动实时轨迹合成
Lockner, E.; Oehlschlägel, T.; Theil et al.
Lockner et al.
Reusability aspects for space transportation rocket engines: programmatic status and outlook [0.03%]
航天运输火箭发动机的可重复使用性方面：项目现状与展望
D. Preclik; R. Strunz; G. Hagemann; G. Langel
D. Preclik; R. Strunz; G. Hagemann; G. Langel
Mars EXPRESS observation of the PHOENIX entry: simulations, planning, results and lessons learned [0.03%]
火星快车对凤凰号的观测：模拟、规划、结果和经验教训
Witasse, O.; Lino da Silva, M.; Sobbia et al.
Witasse et al.
A fluid structure coupling of the Ariane-5 nozzle section during start phase by detached eddy simulation [0.03%]
基于分离涡模拟的阿丽亚娜5号喷管段启动阶段流固耦合研究
Heinrich Lüdeke; Javier B. Calvo
Heinrich Lüdeke; Javier B. Calvo
On the importance of reduced scale Ariane 5 P230 solid rocket motor models in the comprehension and prevention of thrust oscillations [0.03%]
关于缩小比例的阿丽亚娜5号P230固体火箭发动机模型在理解和预防推力振荡中的重要性
J. Hijlkema; M. Prévost; G. Casalis
J. Hijlkema; M. Prévost; G. Casalis
Investigations on the thermal behaviour of CMC-based leading edges in hypersonic arc jet flows [0.03%]
高超声速电弧射流中基于CMC的前缘热行为研究
Kuhn, Markus; Esser, Burkard; Gülhan et al.
Kuhn et al.
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.