Design and Economics of Aircraft
Translation Division, Foreign Technology Division, 1964 - Airplanes - 251 pages
Contents: Weight and aerodynamic improvement of aircraft; Examples of determination of loss from weight and loss from drag; Determination of loss from parameters of aircraft; Determination of expediency of design measures; Examples of increase of efficiency of aircraft; Determination of expenditures on increase of flying characteristics of aircraft; Comparison of efficiency of aircraft of identical assignment; Special cases of determination of loss from weight and loss from drag.
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Efficiency of Aircraft and Ways of Increasing It 17
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aerodynamic drag change of weight Chapter characteristics of aircraft condition of maximum considered aircraft design measures design parameters determination of expenditures determination of loss drag of aircraft economy of means efficiency of aircraft equation of flying expediency of design expenditures of means expenditures on increase find formula find total differential flying characteristics flying range formula for determination formula of loss glider increase of efficiency increase of flying increase of speed increase of thrust increase of weight independent variables kilogram landing speed Let us assume limiting expedient expenditures loss from drag loss from weight maximum of efficiency number of flights parameters of aircraft parasite drag partial derivatives power plant Putting equations quantities relative increases rubles section of flight special purpose load special purpose yield speed of flight tactical characteristics takes form thrust of power unnecessary weight weight and loss weight of aircraft weight of special weight of structure wing area