P. Hennig

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 .

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

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

Navier Stokes Simulation Around a High Velocity Missile with Cross-Flow Jet

P. Hennig, S. M. Hitzel, H. Esch, 1998 .

Heat Transfer at the Nose of a High-Speed Missile

J. Srulijes, P. Hennig, F. Seiler, 2010 .