论文信息 - Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft - 字舞流文

Higher Level Aerodynamic Input for Aeroservoelastic control of Flexible Aircraft

Siva M. Mangalam | Peter Flick | Martin Brenner | M. Brenner | P. Flick | S. Mangalam

[1] Mikhail Goman,et al. State-Space Representation of Aerodynamic Characteristics of an Aircraft at High Angles of Attack , 1994 .

[2] K. K. Gupta,et al. Integrated aeroservoelastic analysis capability with X-29A comparisons , 1989 .

[3] James H. Myatt,et al. Flow Control Research and Applications at the AFRL's Air Vehicles Directorate , 2004 .

[4] Douglas I. Greenwell,et al. A Review of Unsteady Aerodynamic Modelling for Flight Dynamics of Manoeuvrable Aircraft , 2004 .

[5] Carl P. Tilmann,et al. Structural Modal Control and Gust Load Alleviation for a SensorCraft Concept , 2005 .

[6] David Lucia,et al. The SensorCraft Configurations: A Non-Linear AeroServoElastic Challenge for Aviation , 2005 .

[7] S. Kuppa,et al. In-flight detection of flow separation, stagnation, and transition , 1992 .

[8] S. Suryanarayan,et al. Extraction of inherent aerodynamic lag poles for the time domain representation of modal unsteady airloads , 1993 .

[9] Mark H Lowenberg,et al. Comparative Evaluation of Unsteady Aerodynamic Modelling Approaches , 2004 .