DocumentCode
2068620
Title
Aerodynamic Interactions between Adjacent Slender Bodies Instrumentation and Wind Tunnel Testing
Author
Weihs, D. ; Ringel, M. ; Victor, M.
Author_Institution
Technion, Haifa
fYear
2007
fDate
10-14 June 2007
Firstpage
1
Lastpage
28
Abstract
Most externally carried aircraft stores are basically slender bodies. These stores are usually carried underneath the wings or fuselage (itself a slender body) and in many cases multiple bodies are carried in proximity. This proximity introduces new interaction forces, both in the longitudinal and lateral directions. Wind tunnel experiments on a pair of generic slender bodies-ellipsoids of a 6:1 slenderness ratio placed in parallel in the longitudinal direction, at various lateral spacing and axial displacement are described. The results show that significant side and axial forces are obtained. The results are then compared to calculations based on a theoretical model recently applied by the senior author to the interaction of pairs of such slender bodies, with very good agreement, up to the limits of the first order model. When the bodies are positioned correctly, the axial interaction force counters all of the viscous drag on one of the bodies.
Keywords
aerodynamics; aerospace components; aircraft; drag; wind tunnels; adjacent slender bodies instrumentation; aerodynamic interactions; aircraft; axial displacement; axial interaction force; fuselage; slenderness ratio; viscous drag; wind tunnel testing; wings; Aerodynamics; Aerospace electronics; Aerospace engineering; Aerospace testing; Aircraft propulsion; Dolphins; Drag; Ellipsoids; Force measurement; Instruments;
fLanguage
English
Publisher
ieee
Conference_Titel
Instrumentation in Aerospace Simulation Facilities, 2007. ICIASF 2007. 22nd International Congress on
Conference_Location
Pacific Grove, CA
Print_ISBN
978-1-4244-1599-1
Electronic_ISBN
978-1-4244-1600-4
Type
conf
DOI
10.1109/ICIASF.2007.4380899
Filename
4380899
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