J. Birkemeyer

Adapted Wind Tunnel Walls for a Swept Wing Experiment

J. Birkemeyer, 1999 .

APPLICATION OF A 3-D SHOCK CONTROL BUMP ON A TRANSPORT

H. Rosemann, J. Birkemeyer, K. Richter, 2002 .

Active Control Technology for Enhanced Performance Operational Capabilities of Military Aircraft, Land Vehicles and Sea Vehicles

Anuradha M. Annaswamy, G. S. Samuelsen, M. F. Golnaraghi, 2001 .

Flow separation experimental analysis in overexpanded subscale rocket-nozzles

D. Blacodon, J. Birkemeyer, D. Blacodon, 2001 .

Shock Control by Adaptive Elements for Transportation Aircraft Wings

H. Rosemann, J. Birkemeyer, H. Rosemann, 2000 .