A multi-disciplinary toolbox for rotorcraft design

The German Aerospace Center (DLR) is currently developing a multidisciplinary toolbox for the design of conventional and unconventional rotorcraft. The resulting design process will be the result of the DLR-internal project EDEN (Evaluation and DEsign of Novel rotorcraft concepts), which is a joint study between the Institute of Flight Systems, the Institute of Aerodynamics and Flow Technology and the Institute of Structures and Design. The complexity of rotorcraft design requires the development of the tools directly by the specialists of the respective institutes, where the tools are continuously refined and published to authorized users. The integration of the tools into a suitable software framework and the harmonization of the tools among each other are presented. This framework delivers a high level of modularity making the layout and testing of the process very flexible. The implemented tools cover the conceptual and preliminary design phases. The design process starts with an empty workspace and the minimum input of payload mass, range, cruise speed, number of rotor blades and a rotor configuration. Not only conventional main/tail rotor configurations can be designed, but also some other configurations with more than one main rotor. The fundamental concept behind the layout of the tools inside the process is demonstrated, especially the use of scaling and optimization loops. The process includes statistical methods to initialize the dataset, methods with more sophisticated physical models for the scaling task and finite element methods for the best possible prediction of the structural properties quite early in the design process.

[1]  Arne Bachmann,et al.  Automation of Aircraft Pre-design Using a Versatile Data Transfer and Storage Format in a Distributed Computing Environment , 2009, 2009 Third International Conference on Advanced Engineering Computing and Applications in Sciences.

[2]  Martin Siemann,et al.  A parametric aircraft fuselage model for preliminary sizing and crashworthiness applications , 2016 .

[3]  M. Powell A View of Algorithms for Optimization without Derivatives 1 , 2007 .

[4]  Daniel P. Raymer,et al.  Aircraft Design: A Conceptual Approach , 1989 .

[5]  Philipp Kunze Parametric Fuselage Geometry Generation and Aerodynamic Performance Prediction in Preliminary Rotorcraft Design , 2013 .

[6]  Daniel,et al.  Helicopter Design Cost Minimization using Multidisciplinary Design Optimization , 2007 .

[7]  Arne Bachmann,et al.  Advances in Generalization and Decoupling of Software Parts in a Scientific Simulation Workflow System , 2010 .

[8]  W. von Grünhagen,et al.  HOST, a General Helicopter Simulation Tool for Germany and France , 2000 .

[9]  Dieter Kohlgrüber,et al.  A FINITE ELEMENT BASED TOOL CHAIN FOR STRUCTURAL SIZING OF TRANSPORT AIRCRAFT IN PRELIMINARY AIRCRAFT DESIGN , 2013 .

[10]  Martin Siggel The TiGL Geometry Library , 2013 .

[11]  Dimitrios Palasis Erstellung eines Vorentwurfsverfahrens für Hubschrauber mit einer Erweiterung für das Kipprotorflugzeug , 1992 .

[12]  Robert T. N. Chen A survey of nonuniform inflow models for rotorcraft flight dynamics and control applications , 1990 .

[13]  Raymond W. Prouty,et al.  Helicopter performance, stability, and control , 1986 .

[14]  P. M. Fischer,et al.  Open source software framework for applications in aeronautics and space , 2012, 2012 IEEE Aerospace Conference.

[15]  J. Gordon Leishman,et al.  Principles of Helicopter Aerodynamics , 2000 .

[16]  Carsten M. Liersch,et al.  A distributed toolbox for multidisciplinary preliminary aircraft design , 2011 .