Military aeroplanes; an explanatory consideration of their characteristics, performances, construction, maintenance, and operation, for the use of aviators . 0 4 C° S /O /^ /<? /^ /S ^C ^sa ^<Z JE% ^3 JfC/^NQLES or TnciPENCB. 9o. ^ .:5 C 7 CFKACtic^/cf CHOfiD) .6 AC Curve 6, shows the coefficients for Lift, and the vahies of I. D, for arcs of 1/7,1 and 1/27 camber, and the reverse curve section. Curve 7, sliows tlie c. j). nioxriiuiit for tlie same sections. 07 Aerofoils. Unl\ Hal and the siinplcsL ^^omclrical sections have been con-sidered here. In aeroplane wings, it i
Military aeroplanes; an explanatory consideration of their characteristics, performances, construction, maintenance, and operation, for the use of aviators . 0 4 C° S /O /^ /<? /^ /S ^C ^sa ^<Z JE% ^3 JfC/^NQLES or TnciPENCB. 9o. ^ .:5 C 7 CFKACtic^/cf CHOfiD) .6 AC Curve 6, shows the coefficients for Lift, and the vahies of I. D, for arcs of 1/7,1 and 1/27 camber, and the reverse curve section. Curve 7, sliows tlie c. j). nioxriiuiit for tlie same sections. 07 Aerofoils. Unl\ Hal and the siinplcsL ^^omclrical sections have been con-sidered here. In aeroplane wings, it is necessary to have spars andribs of considerable dci)th, in order to obtain suitable strength andrigidity of wing. This leads to sections of surfaces in which two cur-vatures must be considered — the to]) face and the bottom face. An aeroplane wing section is, therefore, distinct from geometri-cal sections, and it is customary to refer to aeroplane types of sur-faces as Aerofoils. They are treated of fully in Chapter VII, sincea knowledge of their characteristics, advantages and disadvantagesenables the first essential step in the design of an aeroplane to be taken —?the choice of a wing section that will give the weight
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Keywords: ., bookcentury1900, bookdecade1910, booksubjectairplanes, bookyear19
