Title :
Aerodynamic Interactions between Adjacent Slender Bodies Instrumentation and Wind Tunnel Testing
Author :
Weihs, D. ; Ringel, M. ; Victor, M.
Author_Institution :
Technion, Haifa
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;
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
DOI :
10.1109/ICIASF.2007.4380899