Recent research topics in high-lift aerodynamics

被引：1
作者：
Wild J. [1 ]
机构：
[1] DLR Institute for Aerodynamics and Flow Technology, Lilienthalplatz 7, Brunswick
来源：
CEAS Aeronautical Journal | 2016年 / 7卷 / 03期
关键词：
Active flow separation control; High-lft system noise; High-lift aerodynamics; Laminar wing high-lift;
D O I：
10.1007/s13272-016-0206-3
中图分类号：
学科分类号：
摘要：
High-lift systems are matured, robust and reliable components of a transport aircraft. Although facing nearly 100 years of history, there is an ongoing need of research in the aerodynamics of such systems due to changes in the requirements for aircraft development. Other than in former times, high-lift aerodynamics research is nowadays more incorporated into larger projects. It is, therefore, not as visible as before when dedicated high-lift projects were conducted, as e.g., the EC funded project EUROLIFT. The aim of this summary is to collect from different projects, the current challenging research topics in the area of high-lift aerodynamics. The contribution gives an overview on recent research topics addressed at the German DLR Institute of Aerodynamics and Flow Technology in collaboration with national and international partners. © 2016, Deutsches Zentrum für Luft- und Raumfahrt e.V.
引用
收藏
页码：345 / 355
页数：10
相关论文
共 34 条
[1]  
Prandtl L., Über Flüssigkeitsbewegung bei sehr kleiner Reibung, Verhandlungen des III. Internationalen Mathematiker-Kongresses Heidelberg, (1905)
[2]  
Nayler J.L., Stedman E.W., Stern W.J., Experiments on an aerofoil having a hinged rear portion. Aeronautical Research Committee (ARC), Reports and Memoranda (R&M), (1914)
[3]  
Lachmann G., Unterteilte Flächenprofile und ihre Bedeutung für die Flugtechnik, (1923)
[4]  
Handley Page F., Wing and similar member of aircraft, US patent 1.353, (1920)
[5]  
Fowler H.D., Aerofoil, US patent 1.670, (1927)
[6]  
Bolkow L., Tragflügel mit Mitteln zur Veränderung der Profileigenschaft, Patentschrift Nr. 694916, Reichspatentamt, (1939)
[7]  
Kruger W., Über eine neue Möglichkeit der Steigerung des Höchstauftriebes von Hochgeschwindigkeitsprofilen, AVA-Bericht 43/W/64, (1943)
[8]  
Smith A.M.O., High-lift system aerodynamics, J. Aircraft, 12, 6, pp. 501-530, (1975)
[9]  
European aeronautics: a vision for 2020, Office for Official Publications of the European Communities, (2001)
[10]  
Flightpath 2050—Europe’s vision for aviation, Publications Office of the European Union, (2011)
1234