Problem considered from point of view of balance that must exist between potential and kinetic energy change of aircraft, energy dissipated against drag, and energy derived from fuel; application of energy approach to problems of climb and range; analytical expression relating change in flight altitude to change in gross weight.
Energy approach to general aircraft performance problem
J Aeronautical Sciences
Journal of the Aeronautical Sciences ; 21 , n 3
1954
9 pages
Article (Journal)
English
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