Wing configuration is a parameter that affects the performance of wing-in-ground effect (WIG) craft. In this study, the aerodynamic characteristics of a new compound wing were investigated during ground effect. The compound wing was divided into three parts with a rectangular wing in the middle and two reverse taper wings with anhedral angle at the sides. The sectional profile of the wing model is NACA6409. The experiments on the compound wing and the rectangular wing were carried to examine different ground clearances, angles of attack, and Reynolds numbers. The aerodynamic coefficients of the compound wing were compared with those of the rectangular wing, which had an acceptable increase in its lift coefficient at small ground clearances, and its drag coefficient decreased compared to rectangular wing at a wide range of ground clearances, angles of attack, and Reynolds numbers. Furthermore, the lift to drag ratio of the compound wing improved considerably at small ground clearances. However, this improvement decreased at higher ground clearance. The drag polar of the compound wing showed the increment of lift coefficient versus drag coefficient was higher especially at small ground clearances. The Reynolds number had a gradual effect on lift and drag coefficients and also lift to drag of both wings. Generally, the nose down pitching moment of the compound wing was found smaller, but it was greater at high angle of attack and Reynolds number for all ground clearance. The center of pressure was closer to the leading edge of the wing in contrast to the rectangular wing. However, the center of pressure of the compound wing was later to the leading edge at high ground clearance, angle of attack, and Reynolds number.
Experimental Aerodynamic Characteristics of a Compound Wing in Ground Effect
Contributed by the Fluids Engineering Division of ASME for publication in the JOURNAL OF FLUIDS ENGINEERING. Manuscript received February 17, 2013; final manuscript received January 28, 2014; published online March 18, 2014. Assoc. Editor: Sharath S. Girimaji.
- Views Icon Views
- Share Icon Share
- Cite Icon Cite
- Search Site
Jamei, S., Abdul Malek, A. M., Mansor, S., Che Sidik, N. A., and Priyanto, A. (March 18, 2014). "Experimental Aerodynamic Characteristics of a Compound Wing in Ground Effect." ASME. J. Fluids Eng. May 2014; 136(5): 051206. https://doi.org/10.1115/1.4026618
Download citation file:
- Ris (Zotero)
- Reference Manager