Enhanced Airfoil Design Incorporating Boundary Layer Mixing Devices
Hybrid Wing Body Model Identification Using Forced-Oscillation Water Tunnel Data (AIAA 2014-2197)
Photoelastic Investigations by means of Stereolithography
Automatisierte, End-of-Line-fahige Prufung des Sitzkomforts und des H-Punkts von Fahrzeugsitzen
Rotary-Balance and Static Wind Tunnel Tests of Forebody Vortex Control Techniques on an F/A-18
Rotary-Balance Test Comparisons with AGARD WG-16 Generic Fighter Model
Forebody Vortex Control on an F/A-18 in a Rotary Flow Field
US/UK Rotary-Balance Test Comparisons with a Generic Fighter Model
US/UK Rotary-Balance Test Comparisons With A Generic Fighter Model
Forebody Vortex Control on an F/A-18 in a Rotary Flow Field