Author:
Übelacker Simon,Hain Rainer,Kähler Christian J.
Publisher
Springer International Publishing
Reference4 articles.
1. Klein, S., Hoppmann, D., Scholz, P., Radespiel, R.: High-Lift Airfoil Interacting with a Vortical Disturbance: Wind-Tunnel Measurements. AIAA Journal, 1–12 (2014), doi:
10.2514/1.J053441
2. Schulze, S.: Experimental Investigations on the Vortex Dynamics of a Stalling Jet Engine Inlet. PhD thesis, Universität der Bundeswehr München, Aeronautics and Astronautics Dept. (2013), ISBN: 978-3-8440-1644-4
3. Vollmers, H.: Detection of vortices and quantitative evaluation of their main parameters from experimental velocity data. Measurement Science & Technology 12, 1199–1207 (2001)
4. Wartzek, F., Holzinger, F., Brandstetter, C., Schiffer, H.P.: Realistic inlet distortion patterns interacting with a transonic compressor stage. In: 4th International Symposium ‘Simulation fo Wing and Nacelle Stall’, Braunschweig, Germany, pp. 1–2. Springer, December 2014
Cited by
11 articles.
订阅此论文施引文献
订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献