D. Wiedmann

发表

Neue Wege bei der Wärmebehandlung und Oberflächenbehandlung hochbelasteter Luftfahrt-Getriebebauteile

J. Kleff, D. Wiedmann, 2000 .

Progress in Combustion and Heat Transfer Modelling in Rocket Thrust Chamber Applied Engineering

M. Frey, D. Wiedmann, Josef Gorgen, 2009 .

Improved heat transfer prediction engineering capabilities for rocket thrust chamber layout

D. Wiedmann, O. Knab, C. Maeding, 2011 .

LOX/Hydrocarbon Propellant Trade Considerations for Future Reusable Liquid Booster Engines

Ludwig Brummer, P. Vuillermoz, Gerald Hagemann, 2005 .

Assessment of different continuum damage models for life-time prediction of high-thrust cryogenic combustion chambers

W. Schwarz, D. Wiedmann, S. Schwub, 2011 .

Weniger Verzug beim Härten durch Computersimulation

D. Wiedmann, G. Schmitt, G. Besserdich, 1999 .

Life prediction of thermally highly loaded components: modelling the damage process of a rocket combustion chamber hot wall

D. Wiedmann, K. Quering, S. Schwub, 2011, CEAS 2011.

Cryogenic rocket calorimeter chamber experiments and heat transfer simulations

Dieter Preclik, D. Wiedmann, W. Oechslein, 1998 .