Fuselage Loads is a structural engineering construct that denotes the aggregate of internal and external forces and moments acting upon an aircraft’s fuselage during flight and ground operations, distinguished by their direct influence on fuselage integrity, deformation, and fatigue within the broader category of airframe load factors.
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Analytical Fuselage and Wing Weight Estimation of Transport Aircraft
Mark D. Ardema, Mark C. Chambers, Anthony P. Patron et al. · ROSA P · 1996 · 100 citations · Full text
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Langley Research Center
Hampton, United States
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Ames Research Center
Mountain View, United States
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165 citations
Boeing (United States)
Chicago, United States
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77 citations
University of Minnesota System
Minneapolis, United States
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Korea Aerospace Research Institute
Daejeon, South Korea
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Santa Clara University
Santa Clara, United States
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144 citations
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Waterloo, Canada
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University of Cambridge
Cambridge, United Kingdom
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