Wind Tunnel Tests for Separation Dynamics Modeling of a Two-Stage Hypersonic Vehicle
International Space Planes and Hypersonic Systems and Technologies Conference (10th]
AIAA Paper 2001-1811
2001
Aerodynamic Active Vibration Alleviation For Buffet Excited Vertical Tails
RTO/AVT Symposium on Advnaced Flow Managment, Part A: Vortex Flows and High Angle of Attack
2001
Investigations On vortex-Induced Vertical Tail Buffeting and Suppression
pp. 535-546
International forum On Aeroelasticity and Structural Dynamics [IFASD]
2001
charakteristik von Seitenleitwerks-Buffetlasten im Stall- und Post-Stall-Bereich
Deutscher Luft- und Raumfahrtkongress [DGLR-2001-068]
2001
Analysis of Turbulent Wake Vortex Behand a large Transport Aircraft in Landing Configuration
Deutscher Luft- und Raumfahrztkongress [DGLR-2001-178]
2001
windkanalversuche zum Trennvorgang eines zweistufigen Hyperschall-Flugsystems
Deutscher Luft- und Raumfahrtkongress [DGLR-2001-165]
2001
Lateral-Directional Coupling and Unsteady Aerodynamic Effects of Hypersonc Vehicles
AIAA Journal of Spacecraft and Rockets
2001
Vol. 38, No. 2
pp. 159-167
Vortical Flowfield Structure at Forward Swept Wing Configurations
AIAA Journal of Aircraft
2001
Vol. 38, No. 2
pp. 193-207
Study on dynmic mechanism of cellular structure
High-pressure Physics (in chinese)
2001
15
pp. 205-214
The variation of the gaseous detonation wave through the cell
Journal of Beijing Institute of Technology (in chinese)
2001
21
pp. 286-291