N. Kroll

发表

Mehrgitterverfahren mit spezieller Vergroeberungsvorschrift zur Berechnuug von reibungsbehafteten Hyperschallstroemungen mit hoher Genauigkeit.

R. Radespiel, N. Kroll, 1990 .

Convergence for Increasing Numbers of Blocks

Cornelis W. Oosterlee, S. Leicher, B. Steckel, 1999 .

A common European Euler code for the analysis of the helicopter rotor flowfield

Ken Badcock, Christian B Allen, Luigi Vigevano, 2000 .

Numerical Simulation in the DLR Institute for Design Aerodynamics

N. Kroll, 1993 .

MEGAFLOW - Numerical Flow Simulation for Aircraft Design Results of the second phase of the German CFD initiative MEGAFLOW, presented during its closing syposium at DLR, Braunschweig, Germany, December 10 and 11, 2002

N. Kroll, J. K. Faßbender, 2005 .

Selected CFD Activities at DLR

N. Kroll, W. Kordulla, H. Schutz, 1993 .

A quadrilateral based second-order TVD method for unstructured adaptive meshes

N. Kroll, M. Aftosmis, N. Kroll, 1991 .

EROS: A European Euler Code For Helicopter Rotor Flow Simulations

Christian B Allen, Luigi Vigevano, L. Morino, 1998 .

Survey of CFD Activities in the DLR Institute for Design Aerodynamicsfor Helicopter Related Problems.

K. Pahlke, N. Kroll, 1992 .

Helicopter Fuselage Drag Prediction: State of the art in Europe

Michel Costes, H. von Geyr, N. Kroll, 2001 .

Selected CFD Activities at DLR(Proceedings of the 11th NAL Symposium on Aircraft Computational Aerodynamics)

N. Kroll, W. Kordulla, H. Schutz, 1994 .

Extension of the Navier-Stokes Code CEVCATS to Hypersonic Equilibrium Flows.

R. Radespiel, N. Kroll, 1992 .

MEGAFLOW - An Industrial Flow Simulation Tool for Aircraft Applications

N. Kroll, 2002 .

Computation of the flow fields of propellers and hovering rotors

N. Kroll, 1986 .

Grid Generation for Multi-Blades and Calculation with a 3D Euler-Code for Helicopter Rotors in Hover

K. Pahlke, N. Kroll, 1991 .

Parallel Large Scale Computations for Aerodynamic Aircraft Design with the German CFD System MEGAFLOW

S. Melber, Ralf Heinrich, B. Schöning, 2002 .

Numerical Grid Generation Techniques

N. Kroll, 1992 .

Capability of State-of-the-Art Navier-Stokes Solvers for the Prediction of Helicopter Fuselage Aerodynamics

Jens Nørkær Sørensen, Michel Costes, H. von Geyr, 1998 .

MEGAFLOW - A numerical Simulation Tool for Aircraft Design

R. Heinrich, N. Kroll, 2004 .

Navier-Stokes Calculations of Helicopter Fuselage Flowfield and Loads

Onera, Agusta, Michel Costes, 1998 .

Multigrid Scheme with Semicoarsening for Accurate Computations of Hypersonic Viscous Flows

R. Radespiel, N. Kroll, 1991 .

Accurate flux vector splitting for shocks and shear layers

Rolf Radespiel, N. Kroll, N. Kroll, 1995 .

An Improved Flux Vector Split Discretization Scheme for Viscous Flows.

R. Radespiel, N. Kroll, N. Kroll, 1994 .

Assessment of Preconditioning Methods

Eli Turkel, Rolf Radespiel, N. Kroll, 1995 .