Phugoid motions in compressible range are defined assuming that thrust is equal to drag and moments about aircraft center of gravity equal zero; under these conditions, both incidences for constant elevator settings, and fuel admission are functions of Mach number; elements of motion and equation of path are deduced with respect to incompressible range.
Phugoid paths of high-speed aircraft
Rev de Mecanique Appliquee
Revue de Mecanique Appliquee ; 6 , n 2
1961
15 pages
Article (Journal)
English
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