Based on typical payload and density variations, method is presented for calculation of achieved payload for available aircraft volume and maximum payload; application of concept to economic evaluation of change to aircraft's design volume shown; methods described are used at Canadair in evaluating operating economics of Cl-44D4 cargo aircraft and its future developments.
Economic evaluation of design volume and payload of cargo aircraft
Can Aeronautical J
Canadian Aeronautical Journal ; 7 , n 2
1961
5 pages
Aufsatz (Zeitschrift)
Englisch
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