K. W. Naumann

SOLID ROCKET PROPULSION FOR THE GERMAN HFK (HYPERSCHALL- FLUGKO RPER) HYPERVELOCITY MISSILE PROGRAM AN OVERVIEW

K. W. Naumann, Bayern-Chemie Protac, 2003 .

A novel technique for aerodynamic force measurement in shock tubes

K. W. Naumann, H. Ende, G. Mathieu, 2008 .

Millisecond Aerodynamic Force Measurement Technique for High-Enthalpy Test Facilities

K. W. Naumann, H. Ende, G. Mathieu, 1993 .

A novel technique for aerodynamic force measurement in shock tubes

K. W. Naumann, H. Ende, 1989, International Congress on Instrumentation in Aerospace Simulation Facilitie.

Bow Shock Wave Heating and Ablation of a Sharp-Nosed Projectile Flying inside a Ram Accelerator

K. W. Naumann, F. Seiler, 1995 .

Millisecond aerodynamic force measurement with side-jet model in theISL shock tunnel

K. W. Naumann, H. Ende, G. Mathieu, 1993 .

Ram Accelerator Ballistic Range Concept for Softly Accelerating Hypersonic Free-Flying Models

Adam P. Bruckner, K. W. Naumann, A. Bruckner, 1994 .