Delta wing steady pressure investigations for sharp and rounded leading edges

Notes on Numerical Fluid Mechanics and Multidisciplinary Design

Volumn 92, Issue , 2006, Pages

  Furman, Andrej ^a   Breitsamter, Christian ^a  

^a TECHNICAL UNIVERSITY OF MUNICH   (Germany)

Author keywords

[No Author keywords available]

Indexed keywords

EID: 84872821818     PISSN: 16122909     EISSN: None     Source Type: Book Series    
DOI: 10.1007/978-3-540-33287-9_10     Document Type: Article

References (6)

1. C. Breitsamter: "Turbulente Strömungsstrukturen an Flugzeugkonfigurationen mit Vorderkantenwirheln". Dissertation, Technische Universität München, Herbert Utz Verlag, ISBN 3-89675-201-4, 1997.
2. J. Chu, J. M. Luckring: "Experimental Surface Pressure Data Obtained on 65° Delta Wing Across Reynolds Nummber and Mach Nummber Ranges". NASA-TM- 4645, Volume 1 -Sharp Leading Edge, 1996.
3. F. Ghafarri: RTO-MP-AVT-113, Personal communication, 2004.
4. D. Hummel, G. Redeker: "A new vortex flow experiment for computer code validation". Paper 8, RTO Symposium on Advanced Flow Management, Part A-Vortex flow and high angle of attack, Leno, Norway, 7-11 May 2001.
5. D. Hummel: "Effects of boundary layer formation on the vortical flow above slender delta wing". Paper 30, RTO Symposium on Enhancement of NATO Military Flight Vehicle Performance by Management of Interacting Boundary Layer Transition and Separation, Prague, Czech Republic, 4-7 Oct. 2004.
6. th Congress of the International Council of the Aeronautical Sciences, Yokohama, Japan, 29 Aug.-3. Sept. 2004.