Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-Lift Wing-Reference-Cited by-同舟云学术

Impact of Different UHBR-Engine Positions on the Aerodynamics of a High-Lift Wing

Published:2015-07-10 Issue: Volume: Page:367-380
ISSN:1612-2909
Container-title:Notes on Numerical Fluid Mechanics and Multidisciplinary Design
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Author:

Ritter Sebastian

Publisher

Springer International Publishing

Link

http://link.springer.com/content/pdf/10.1007/978-3-319-21127-5_22

Reference10 articles.

1. European Commission et al. Flightpath 2050. Europe’s Vision for Aviation. Report of the High Level Group on Aviation Research (2011)

2. Dirk M.: Franke. Multidisciplinary optimization of a generic 2d high-lift configuration regarding kinematics, aerodynamics and flight mechanics. AIAA-Paper-No. 2012–3017 (June 2012)

3. Bundesministerium für Wirtschaft und Energie. Luftfahrtforschungsprogramm des Bundes (LuFo) (July 2014). http://www.bmwi.de (visited on July 3, 2014)

4. Gerhold, T., Friedrich, O., Evans, J., Galle, M.: Calculation of complex three-dimensional configurations employing the DLR-TAU-code. AIAA paper 167, 10 (1997). AIAA-Paper-No. 97–0167

5. Kallinderis, Y., Khawaja, A., McMorris, H.: Hybrid prismatic/tetrahedral grid generation for viscous flows around complex geometries. AIAA Journal 34(2), 291–298 (1996)

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