TY - JOUR
T1 - Delta wing steady pressure investigations for sharp and rounded leading edges
AU - Furman, Andrej
AU - Breitsamter, Christian
PY - 2006
Y1 - 2006
N2 - The design, construction, manufacturing and geometric properties of a generic 65° Delta Wing for the International Vortex Flow Experiment 2 are described. Briefly, the measurement equipment implemented in the model and the external sensors are specified. A wind tunnel investigation has been performed and the results for two different leading edge geometries (sharp and rounded) at three angles of attack are discussed in detail. Further, the results are compared with the ones obtained by NASA and also with computational results. Partly developed (α = 13°) and fully developed (α = 18°) leading edge vortices as well as vortex breakdown (α= 23°) are considered.
AB - The design, construction, manufacturing and geometric properties of a generic 65° Delta Wing for the International Vortex Flow Experiment 2 are described. Briefly, the measurement equipment implemented in the model and the external sensors are specified. A wind tunnel investigation has been performed and the results for two different leading edge geometries (sharp and rounded) at three angles of attack are discussed in detail. Further, the results are compared with the ones obtained by NASA and also with computational results. Partly developed (α = 13°) and fully developed (α = 18°) leading edge vortices as well as vortex breakdown (α= 23°) are considered.
UR - http://www.scopus.com/inward/record.url?scp=84872821818&partnerID=8YFLogxK
U2 - 10.1007/978-3-540-33287-9_10
DO - 10.1007/978-3-540-33287-9_10
M3 - Article
AN - SCOPUS:84872821818
SN - 1612-2909
VL - 92
JO - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
JF - Notes on Numerical Fluid Mechanics and Multidisciplinary Design
ER -