Volume 8, issue 4, December 2017

11 articles in this issue

Support of icing flight tests by near real-time data analysis

Authors
- Christian Raab
- Per Ohme
- Christoph Deiler
- Content type: Original Paper
- Published: 31 August 2017
- Pages: 561 - 577
Adaptive backstepping neural network control for three dimensions trajectory tracking of robotic airships

Authors
- Yueneng Yang
- Wenqiang Wang
- Ye Yan
- Content type: Original Paper
- Published: 04 September 2017
- Pages: 579 - 587
Numerical modelling of the aerodynamic interference between helicopter and ground obstacles

Authors (first, second and last of 4)
- Giulia Chirico
- Damien Szubert
- George N. Barakos
- Content type: Original Paper
- Open Access
- Published: 05 September 2017
- Pages: 589 - 611
Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb

Authors (first, second and last of 4)
- Armin Weiss
- Anthony D. Gardner
- Markus Raffel
- Content type: Original Paper
- Published: 19 September 2017
- Pages: 613 - 623
Flight mechanics model for spanwise lift and rolling moment distributions of a segmented active high-lift wing

Authors (first, second and last of 5)
- J. H. Diekmann
- D. Keller
- V. Gollnick
- Content type: Original Paper
- Published: 20 September 2017
- Pages: 625 - 635
In-flight tracking and vibration control using the DLR’s multiple Swashplate system

Authors
- Philip M. Küfmann
- Claudio Brillante
- Content type: Original Paper
- Published: 03 October 2017
- Pages: 637 - 652
Aileron endurance test rig design based on high fidelity mathematical modeling

Authors
- Mukesh Prasad
- K. V. Gangadharan
- Content type: Original Paper
- Published: 07 October 2017
- Pages: 653 - 671
Multidisciplinary optimization of an NLF forward swept wing in combination with aeroelastic tailoring using CFRP

Authors (first, second and last of 4)
- Tobias Wunderlich
- Sascha Dähne
- Lars Reimer
- Content type: Original Paper
- Published: 10 October 2017
- Pages: 673 - 690
Benefit evaluation of hybrid electric propulsion concepts for CS-23 aircraft

Authors
- M. Kreimeier
- E. Stumpf
- Content type: Original Paper
- Published: 14 October 2017
- Pages: 691 - 704
Edge-based approach to estimate the drift of a helicopter during flight

Authors
- Alexander Gatter
- Content type: Original Paper
- Published: 27 October 2017
- Pages: 705 - 718
Multi-use 48-kW power electronics for future aerospace applications

Authors (first, second and last of 4)
- Rodolphe De Maglie
- Alfred Engler
- Ralf Cremer
- Content type: Short Communication
- Published: 23 October 2017
- Pages: 719 - 726

Volume 8, issue 4, December 2017

Support of icing flight tests by near real-time data analysis

Adaptive backstepping neural network control for three dimensions trajectory tracking of robotic airships

Numerical modelling of the aerodynamic interference between helicopter and ground obstacles

Boundary-layer transition measurements on Mach-scaled helicopter rotor blades in climb

Flight mechanics model for spanwise lift and rolling moment distributions of a segmented active high-lift wing

In-flight tracking and vibration control using the DLR’s multiple Swashplate system

Aileron endurance test rig design based on high fidelity mathematical modeling

Multidisciplinary optimization of an NLF forward swept wing in combination with aeroelastic tailoring using CFRP

Benefit evaluation of hybrid electric propulsion concepts for CS-23 aircraft

Edge-based approach to estimate the drift of a helicopter during flight

Multi-use 48-kW power electronics for future aerospace applications

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Volume 8, issue 4, December 2017

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