Scientific Commons: G. Koppenwallner

Effects of Propulsive Jet on the Flow Field in the Tail Region of a Missile in a Supersonic Stream, (9999)

Koppenwallner,G., Rammenzweig,D., Stahl,W.

This article work concentrated on the effects of an under-expanded supersonic jet on the external supersonic flow past a typical missile configuration. Jet simulation in the wind tunnel was achieved...

THE PRINCETON UNIVERSITY HIGH PRESSURE HYPERSONIC NITROGEN TUNNEL N-3. PART I. FACILITY DESCRIPTION. PART II. CALCULATION OF GAS CHARACTERISTICS AND EVALUATION OF EFFECTS OF VIBRATIONAL NON-EQUILIBRIUM. PART III. PRELIMINARY MEASUREMENTS, (2005)

VAS,I. E., Koppenwallner,G.

A hypersonic wind tunnel using nitrogen as the test fluid was built to operate in the continuum and slip flow regimes. The free stream Mach number in the 6-8 inch diameter test section varies from...

MOP: A space debris and interplanetary dust sample return mission. (1999)

Kaldeich-Schürmann, B., Scherer, K., Hilchenbach, M., Kirsch, E., Livi, S., Bendisch, J., ...

MOP: A space debris and interplanetary dust sample return mission. (1999)

Scherer, K., Hilchenbach, M., Kirsch, E., Livi, S., Bendisch, J., Blum, J., ...

ParBoSS - Ein anwendungsorientiertes massiv paralleles Simulationstool für Strömungen in verdünnten Gasen (1997)

Struckmeier, J., Antonov, S., Koppenwallner, G., Schüller, A.

Integrated Measurement System for a Hypersonic Experimental Vehicle. (1996)

Koschel, W., Janovsky, R.(1), Koppenwallner, G.(2), Kovaltschuk, V. (3)

German Reentry Experiments on " Express " (1994)

Koppenwallner, G.

Calibration and First Results of a Redesigned LUDWIEG-Expansion Tube. (1993)

Friehmelt, H., Koppenwallner, G. (1), Müller-Eigner, R. (2)