Control of Wing-Engine-Slat Cut Out Flow Separation Using Nacelle Nozzle Modification

Author:

Cui Zheng,Wang Jiangang,Du Xi,Lin Dakai,Cao Yihua

Publisher

Springer Nature Singapore

Reference10 articles.

1. Monat S, Maayan P, Bar M, Ariel Y, Avraham S, Ofek D (2020) Suction and pulsed blowing for control of local wing-engine-slat-cut out flow separation: the INAFLOWT project. In: AIAA 2020 Aviation Forum. AIAA 2020-2953

2. Bangmeng X et al (2018) Multi-Objective Wing Optimization of Civil Aircrafts in Engine-Aircraft Integration Configuration. Acta Aerodynamica Sinica 36(6):941–948

3. Adam J, Oliver A (2009) Design of a High-Lift System with Droop Nose Device. Journal of Aircraft 46:731–734

4. Michael PP, Jochen W W, Lothar B (2014) Aerodynamic and Acoustic Design of Silent Leading Edge Devices. In: 20th AIAA/CEAS Aeroacoustics Conference. AIAA 2014-2076

5. Hans M, Markus K et al (2009) Design of a Smart Droop Nose as Leading Edge High Lift System for Transportation Aircrafts. 50th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. AIAA 2009-2128

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