D. Rammenzweig

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...

Heat Transfer Measurements on a Blunted 70 Deg Half Angle Cone in High Enthalpy Small Reynolds Number Flow (1995)

Legge, H., Rammenzweig, D., Klotzbach, A.

The heat transfer, especially at the stagnation point, of a generic ASTV (Aeroassist Space Transfer Vehicle) configuration, i.e. a 70 degree half angle blunted cone, is measured on "mini...

Calibration Data of V2G with a Conical Ma = 15 Nozzle (1994)

Legge, H., Von Roden, G., Klotzbach, A., Rammenzweig, D.

The flow in the vacuum wind tunnel V2G Goettingen with a 15 deg half angle conical nozzle, 400 mm test section diameter, and Ma = 15 is calibrated by Pitot pressure measurements. The flow is...