P. Krogmann

发表

Investigation of Three-dimensional Hypersonic Boundary Layer Structures at the Flaps of Reentry Vehicles

H. Lüdeke, P. Krogmann, 2000 .

Method for High Speed Turbulent Separated Flows with Experimental Verification

M. Ravachol, Arne V. Johansson, Stefan Wallin, 1998 .

Investigation of the Turbulent Flow Past a Blunt Fin/Wedge Configuration

T. Gerhold, P. Krogmann, 1993 .

An experimental study of boundary layer transition on a slender cone at Mach 5

P. Krogmann, P. Krogmann, 1977 .

An experimental investigation of laminar and transitional heat transfer to a sharp slender cone at free-stream Mach number 5, including effects of angle of attack and circumferential heat transfer

P. Krogmann, 1974 .

Active and Passive Shock/Boundary Layer Interaction Control on Supercritical Airfoils,

E. Stanewsky, P. Krogmann, P. Thiede, 1984 .

Investigation of the hypersonic turbulent flow past a blunt fin/wedge configuration

T. Gerhold, P. Krogmann, 1993 .