On the basis of the assumption that the external stores are small compared with the wing, an approximate method has been developed for estimation of two-dimensional apparent masses for the cross-flow sections of wing-store combinations. The results obtained may be applicable to the analysis of the effects of the stores on the aerodynamic stability derivatives in slender-body theory. The theory has also been applied to estimate the rolling moment due to sideslip for high-wing configurations. The presented results are in agreement with those of other investigations.
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Two-Dimensional Apparent Masses for Cross-Flow Sections of Wing-Store Configurations
Nanjing Aeronautical Institute, Nanjing, Jiangsu, People’s Republic of China
Huang, M. (September 1, 1982). "Two-Dimensional Apparent Masses for Cross-Flow Sections of Wing-Store Configurations." ASME. J. Appl. Mech. September 1982; 49(3): 471–475. https://doi.org/10.1115/1.3162483
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