The rocket sled system is not only a high-speed dynamic ground test system,but also one of the future aerospace horizontal launch schemes.The winged load,as a common type of payload,has greater vibration and noise int...The rocket sled system is not only a high-speed dynamic ground test system,but also one of the future aerospace horizontal launch schemes.The winged load,as a common type of payload,has greater vibration and noise intensity than the wingless load.Due to the severe aerodynamic instability prior to separation,the head-up or head-down phenomena are more evident and the test accuracy significantly decreases.The high-precision computer fluid dynamics and aeroacoustic analysis are employed to explore the multifield coupling mechanism of a rocket sled with the winged payload in the wide speed range(Ma=0.5–2).The results show that as the incoming velocity increases,the cone angle of the shock wave of the rocket sled decreases,the shock pressure increases quickly,and the vortex between the slippers splits and gradually shrinks in size.The velocity of the rocket sled exerts little influence on the modal resonance frequency.The wing has a significant impact on aerodynamic noise,and as the sound pressure level rises,the propagation direction gradually shifts towards the rear and upper regions of the wing.展开更多
当前IMS Learning Design(IMS LD)规范中虽然整合了QTI(Question and Test Interoperability)规范,但是在当前的播放器中却没有很好地整合QTI服务,这就阻碍了播放器和QTI之间的通信,从而不能很好地实现QTI服务。文中针对SLeD体系结构,...当前IMS Learning Design(IMS LD)规范中虽然整合了QTI(Question and Test Interoperability)规范,但是在当前的播放器中却没有很好地整合QTI服务,这就阻碍了播放器和QTI之间的通信,从而不能很好地实现QTI服务。文中针对SLeD体系结构,在该体系结构中加入了中间软件层,利用这个中间软件层实现了播放阶段QTI和播放器的通信。展开更多
基金supported by the National Natural Science Foundation of China(No.12104047)。
文摘The rocket sled system is not only a high-speed dynamic ground test system,but also one of the future aerospace horizontal launch schemes.The winged load,as a common type of payload,has greater vibration and noise intensity than the wingless load.Due to the severe aerodynamic instability prior to separation,the head-up or head-down phenomena are more evident and the test accuracy significantly decreases.The high-precision computer fluid dynamics and aeroacoustic analysis are employed to explore the multifield coupling mechanism of a rocket sled with the winged payload in the wide speed range(Ma=0.5–2).The results show that as the incoming velocity increases,the cone angle of the shock wave of the rocket sled decreases,the shock pressure increases quickly,and the vortex between the slippers splits and gradually shrinks in size.The velocity of the rocket sled exerts little influence on the modal resonance frequency.The wing has a significant impact on aerodynamic noise,and as the sound pressure level rises,the propagation direction gradually shifts towards the rear and upper regions of the wing.
文摘当前IMS Learning Design(IMS LD)规范中虽然整合了QTI(Question and Test Interoperability)规范,但是在当前的播放器中却没有很好地整合QTI服务,这就阻碍了播放器和QTI之间的通信,从而不能很好地实现QTI服务。文中针对SLeD体系结构,在该体系结构中加入了中间软件层,利用这个中间软件层实现了播放阶段QTI和播放器的通信。
