F. Leopold

Turbulence Model Studies to Investigate the Aerodynamic Performance of a NASA Dual Control Missile at Supersonic Mach Numbers

Simon Prince, M. Mendenhall, M. Khalid, 2005 .

Wind Tunnel Rig for the Study of Roll Damping and Pitch Damping Effects of Free-Spinning Models at Supersonic Speed

L. Gross, F. Leopold, G. Gastebois, 2005, ICIASF 2005 RecordInternational Congress onInstrumentation in AerospaceSimulation Facilities.

Application of Various Turbulence Models to Investigate the Aerothermodynamic Performance of a NASA Dual Control Missile

Mahmood Khalid, Simon Prince, M. Mendenhall, 2004 .

Schlieren Techniques in Comparison: The Background Oriented Method versus Visualization with Holographic Filters.

Markus Raffel, H. Richard, F. Leopold, 2001 .

Reconstruction of the density field using the Colored Background Oriented Schlieren Technique (CBOS)

F. Leopold, F. Sourgen, D. Klatt, 2012 .

Experimental investigation of shock/vortex interaction for slender canard configurations at supersonic speed

F. Leopold, C. Demeautis, F. Jagusinski, 2003, 20th International Congress on Instrumentation in Aerospace Simulation Facilities, 2003. ICIASF '03..