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Falk Klinge

German Aerospace Center

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Publication

Featured researches published by Falk Klinge.

Archive | 2007

Studies of Reynolds Number Effects on Wing Tip Vortex Positions by Means of Laser Light Sheet (LLS) and Background Oriented Schlieren (BOS) Technique Under Cryogenic Conditions

Dieter Pallek; Falk Klinge

The Background Oriented Schlieren Method (BOS) and the Laser Light Sheet technique (LLS) were successfully adapted to the cryogenic European Transonic Windtunnel (ETW) and applied to wing tip vortex investigations. Applying optical measurement techniques to ETW is difficult, because of the extreme wind tunnel conditions (temperature, pressure, poor optical access).

Archive | 2003

Application of Quantitative Background Oriented Schlieren (BOS): Investigation of a Wing Tip Vortex in a Transonic Wind Tunnel

Falk Klinge; Tania Kirmse; Jürgen Kompenhans

Archive | 2006

Camera calibrating method for optical measuring system, involves marking one of cross-over points in checker pattern by position information, which is readable by image processing of images of pattern and has coding of orientation

Sebastian Gesemann; Falk Klinge

Archive | 2007

Method of detecting the contour of a reflective surface using a virtual image of the reflective points

Erik Dipl.-Ing. Goldhahn; Falk Klinge; Robert Konrath; Andreas Schröder

Archive | 2006

Measurement of the position of rotor blade vortices generated by a helicopter in free flight by means of stereoscopic Background Oriented Schlieren Method (BOS)

Falk Klinge; Martin Hecklau; Markus Raffel; Jürgen Kompenhans; Uwe Göhmann

Archive | 2004

Scheimpflug adapter for connecting a camera to a lens while maintaining the Scheimpflug criterion comprises pivot axes in the image plane of camera that run through a joint ball mid-point

Falk Klinge; Hartmut Mattner; Markus Raffel

Archive | 2005

Surface measurement method e.g. for measuring surface deformations, using angle between projection line of sight and surface or reference surface and angle between illustration line

Falk Klinge; Andreas Schroeder; Markus Raffel; Burkhard Dr.Ing. Binder

Archive | 2004

Investigation of the density and velocity distribution of a wing tip vortex by means of stereoscopic Background Oriented Schlieren Method (BOS) and stereoscopic Particle Image Velocimetry (PIV)

Falk Klinge; Tania Kirmse; Jürgen Kompenhans

Archive | 2005

Reproducing series of derived images of repeating process involves only recording next direct image if it can be evaluated without delay following recording of last image required for respective individual evaluation

Boleslaw Stasicki; Holger Frahnert; Falk Klinge

Archive | 2009

Stochastic point sample measuring method, involves detecting stochastic point sample on surface using camera, and continuing basic pattern with smaller points over larger points of other basic pattern

Falk Klinge; Boleslaw Stasicki

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Collaboration

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Jürgen Kompenhans

German Aerospace Center

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Boleslaw Stasicki

German Aerospace Center

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Andreas Schröder

German Aerospace Center

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Markus Raffel

German Aerospace Center

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Martin Hecklau

Technical University of Berlin

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Robert Konrath

German Aerospace Center

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Sebastian Gesemann

German Aerospace Center

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Dieter Pallek

German Aerospace Center

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Erik Dipl.-Ing. Goldhahn

German Aerospace Center

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Holger Frahnert

German Aerospace Center

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