职业 发表于 2025-3-26 23:37:12
cal method which both allow to establish the existence of transversal homoclinic points is given..Applications are presented for simple mechanical systems like the pendulum with oscillating support, a satellite on an elliptic orbit, a two bar robot performing a prescribed endpoint motion and the claInterstellar 发表于 2025-3-27 03:14:01
rcuitry increases as the number of scrolls does it. On the other hand, discrete active devices cannot tune more than 3 decimals, i.e., due to the high sensitivities of the circuit elements, it is difficult to set coefficient values lower than 0.001. That way, this chapter shows how does an FPGA is u极微小 发表于 2025-3-27 07:48:58
rcuitry increases as the number of scrolls does it. On the other hand, discrete active devices cannot tune more than 3 decimals, i.e., due to the high sensitivities of the circuit elements, it is difficult to set coefficient values lower than 0.001. That way, this chapter shows how does an FPGA is uRUPT 发表于 2025-3-27 10:34:20
patterns, no reconstruction process was performed, as the interest in those cases was in the fringe patterns themselves (the wave progression patterns). Nevertheless, to record acoustic fringe patterns for hologram use, the same technique is applicable, and acoustic holograms and their reconstructioModicum 发表于 2025-3-27 17:30:23
http://reply.papertrans.cn/83/8217/821609/821609_35.png枕垫 发表于 2025-3-27 19:46:42
http://reply.papertrans.cn/83/8217/821609/821609_36.png珊瑚 发表于 2025-3-27 23:04:43
http://reply.papertrans.cn/83/8217/821609/821609_37.pngGobble 发表于 2025-3-28 02:49:23
Elektrische Antriebe,er unkonventionellen Triebwerkstechnologie gegeben werden. Als . können allgemein die folgenden Arten definiert werden: .• Die Energiequelle ist vom Treibstoff getrennt und .• dem Treibstoff wird elektrische Energie zugeführt.MORPH 发表于 2025-3-28 09:59:09
http://reply.papertrans.cn/83/8217/821609/821609_39.png影响带来 发表于 2025-3-28 13:21:47
Die Ziolkowsky-Raketengleichung,n, falls die Austrittsgeschwindigkeit der Raketengase an der Düse und das Verhältnis der Raketenmasse beim Brennschluss zur Startmasse bekannt sind. Umgekehrt kann bei Vorgabe einer gewünschten Geschwindigkeitsänderung der Rakete die dazu notwendige Treibstoffmasse bestimmt werden.