ALLFlight: tackling the brownout problem T. LuekenN. PeineckeR. Lantzsch Original Paper 21 August 2011 Pages: 1 - 15
Engine integration based on multi-disciplinary optimisation technique Danil HaarJoël Brezillon Original Paper 25 August 2011 Pages: 17 - 24
Applications of a discrete viscous adjoint method for aerodynamic shape optimisation of 3D configurations Joël BrezillonRichard P. Dwight Original Paper 28 October 2011 Pages: 25 - 34
Primary structure mass estimation in early phases of aircraft development using the finite element method J. WenzelM. SinapiusU. Gabbert Original Paper 15 November 2011 Pages: 35 - 44
Characterisation of the combustion performance of low emission fuel injectors with laser measurements U. MeierJ. HeinzeT. Doerr Original Paper 20 January 2012 Pages: 45 - 53
Probabilistic endurance level analyses of compressor blades Kay HeinzeSven SchrapeKonrad Vogeler Original Paper 07 February 2012 Pages: 55 - 65
MDO analyses of wing structures for a complete aeroelastically constrained aircraft Franco MastroddiMarco TozziEmanuele Mastrella Original Paper 15 February 2012 Pages: 67 - 77
The influence of engine thrust behaviour on the aerodynamics of engine airframe integration H. HoheiselH. Frhr. von Geyr Original Paper 09 March 2012 Pages: 79 - 92
Extensions of prescribed wake modelling for helicopter rotor BVI noise investigations Berend G. van der Wall Original Paper 11 March 2012 Pages: 93 - 115